ACE : ACE : EPAM : EPAM : 5MINUTE P1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P8 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P8 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE DE1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE DE2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE DE3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE DE4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_DE1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_DE2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_DE3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_DE4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE W8 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_W8 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E1p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E2p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E3p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E4p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP5p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP6p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP7p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E1p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E2p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E3p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E4p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP5p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP6p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP7p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE Z2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE Z2A Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE Z3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE Z4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_Z2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_Z2A Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_Z3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_Z4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P1p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P2p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P3p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P4p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P5p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P6p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P7p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE P8p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P1p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P2p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P3p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P4p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P5p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P6p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P7p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_P8p Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE E4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE FP7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E1 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E2 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E3 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_E4 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP5 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP6 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE unc_FP7 Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : EPAM : EPAM : 5MINUTE livetime Instrument team contact: Dennis Haggerty Phone: (240) 228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Robert Gold Phone: (240) 228-5412 Org: John Hopkins University Applied Physics Laboratory Email: robert.gold@jhuapl.edu 1 1997-08-30 05:00:00 2006-12-27 05:00:00 ACE : ACE : MAG : MAG : MAG ACE RTN Br * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RTN Bt * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RTN Bn * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RTN B * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RTN Delta * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RTN Lambda * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE Bx * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE By * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE Bz * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM Bx * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM By * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM Bz * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE RMS dB * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE B Uncertanity * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE Good Vectors * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE 16 sec Vectors * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE X * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE Y * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSE Z * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM X * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM Y * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : MAG : MAG : MAG ACE GSM Z * Created by the ACE Science Center (ASC) -- * ACE Science Center Level 2 Software Version: 1.4 * ACE Science Center Processing Date/Time: Fri Mar 9 14:34:18 PST 2007 * For more info email us at: asc@srl.caltech.edu * * For MAG, data error is less than 0.1 nT (where nT is nano-Tesla). * * The timing data indicates the start of the integration period in Universal * Time (UT). This virtual contains the averaged Mag data, which are all * stored as 32-bit floats except the number of vectors sensor, which is stored * as a 32-bit integer. The sensors available in this virtual are: * * (These are available under the RTN coordinate system) * * Br - The r component of the magnetic field vector in the RTN * coordinate system in nT * Bt - The t component of the magnetic field vector in the RTN * coordinate system in nT * Bn - The n component of the magnetic field vector in the RTN * coordinate system in nT * Bmag - The <|B|> magnetic field magnitude in nT * Delta - The angle in degrees with 0 at Br/Bt plane + toward Bn * (-90 to +90 degrees), i.e. the RTN latitude * Lambda - The angle in degrees with 0 at Br and + toward Bt * (0 to 360 degrees), i.e. the RTN longitude * * (These are available under the GSE coordinate system) * * Bgse_x - The x component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_y - The y component of the magnetic field vector in the GSE * coordinate system in nT * Bgse_z - The z component of the magnetic field vector in the GSE * coordinate system in nT * * (These are available under the GSM coordinate system) * * Bgsm_x - The x component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_y - The y component of the magnetic field vector in the GSM * coordinate system in nT * Bgsm_z - The z component of the magnetic field vector in the GSM * coordinate system in nT * * dBrms - RMS values of underlying high-resolution measurements in nT. * This is the rms variation of the vector over the time * interval, calculated as follows: * 1) calculate the average magnitude of each of the three * components of the vector, over the time interval. * 2) for each component, average the square of the * difference between the measurement and the average * 3) add the averages from the three components * 4) take the square-root of the result. * i.e. dBrms = sqrt(sum_i<(B_i-)^2>) * For the 16-second averages, dBrms is calculated using the * the highest resolution data (3 vectors/second, from one of * the two sensors). For the 4-minute and hourly averages, the * 16-second averages are used as input to the calculations. * * sigma_B - The variance of |B| over the time interval, in nT. * i.e. sigma_B = sqrt(<(|B|-<|B|>)^2>). * If sigma_B/<|B|> is small, there was little variation during the * time period. If sigma_B/<|B|> is large, there was much variation * during the time period. sigma_B is only calculated for the * 4-minute and hourly averages. It is calculated using the * 16-second averages as input. * * fraction_good - Fraction of the timing period for which there was data * available. * * N_vectors - (32 bit integer) Number of 16 second vectors that were included * in the average for the time period. * * (position of the ACE spacecraft in GSE coordinates) * * pos_gse_x - x component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_y - y component of the position of the ACE spacecraft in GSE * coordinates in km. * pos_gse_z - z component of the position of the ACE spacecraft in GSE * coordinates in km. * * (position of the ACE spacecraft in GSM coordinates) * * pos_gsm_x - x component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_y - y component of the position of the ACE spacecraft in GSM * coordinates in km. * pos_gsm_z - z component of the position of the ACE spacecraft in GSM * coordinates in km. * * The averaging of 16 sec data to form the longer time period data (4 min, * 1 hr, 1 day, and Bartels rotation) is simply: * Average = Sum(Mag data)/(Number of samples) * for the good data during the period. * * The data quality for the period; data of type 2 have been excised (i.e. * replaced with the fill data value -999.9) and marked in the quality field * as follows: * Quality = 0 Normal data * = 1 Spacecraft Maneuver & subsequent high-nutation period * (~4 hr) * = 2 Bad data/missing data * * For daily and Bartels rotation averages, only Bmag data is valid. For Br, * Bt, Bn, Delta, Lambda, Bgse_x, Bgse_y, and Bgse_z, the fill value (-999.9) * is output. Individual vector components on timescales longer than 1 hour * are considered to be potentially misleading and have questionable value at * 1 AU. For this reason, they are not computed. Values of <|B|> may be more * useful, but the user is cautioned to examine the dBrms value for these * intervals as large values of dBrms may indicate significant changes in the * magnetic field during the averaging interval. * * In order to convert to units other than those stored, the VIDF defines * tables. These tables are as follows: * * Table 0: Sensors 0- 3: converts nT to T * Sensors 6-13: converts nT to T * Sensors 16-21: converts km into AU. MAG Instrument team contact: Charles W. Smith Phone: 603-862-0890 Org: UNH Email: chuck@briaxa.sr.unh.edu MAG Principal Investigator: Norman F. Ness Phone: 302-831-8111 Org: Bartol Research Institute/University of Delaware Email: nfness@bartol.udel.edu Fax: (302) 831-1843 1 1997-08-14 12:00:03 2007-03-24 07:28:21 ACE : ACE : SSV2 : SSV2 : HOURLY nHe2 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vHe2 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vC5 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vO6 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vFe10 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vthHe2 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vthC5 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vthO6 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY vthFe10 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY C6to5 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY O7to6 Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY avqC Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY avqO Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY avqFe Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SSV2 : SSV2 : HOURLY FetoO Instrument team contact: Thomas Zurbuchen Phone: 734-647-6835 Org: University of Michigan Email: thomasz@umich.edu Principal Investigator: George Gloeckler Phone: NA Org: University of Michigan Email: gglo@umich.edu 1 1998-02-03 11:57:07 2007-01-01 12:04:19 ACE : ACE : SWEPAM : SWEPAM : 64sION proton_density SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION proton_temp SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION He4toprotons SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION proton_speed SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION x_dot_GSE SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION y_dot_GSE SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION z_dot_GSE SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION x_dot_RTN SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION y_dot_RTN SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION z_dot_RTN SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION x_dot_GSM SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION y_dot_GSM SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION z_dot_GSM SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gse_x SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gse_y SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gse_z SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gsm_x SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gsm_y SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : SWEPAM : SWEPAM : 64sION pos_gsm_z SWEPAM Instrument team contact: Ruth Skoug Phone: (505) 667-6594 Org: Los Alamos National Laboratories Email: rskoug@lanl.gov SWEPAM Principal Investigator: David J. McComas Phone: (210) 522-5983 Org: Southwest Research Institute Email: dmccomas@swri.edu 1 1998-01-23 12:00:31 2007-04-19 12:36:50 ACE : ACE : ULEIS : ULEIS : HOURLY H_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY H_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY H_S3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY H_S4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY H_S5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_H_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_H_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_H_S3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_H_S4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_H_S5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He3_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He3_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_S3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L9 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L10 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L11 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY He4_L12 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_S2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_S3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L9 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L10 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L11 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_He4_L12 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY C_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_C_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY O_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_S1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_O_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Ne_S_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Ne_S_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY Fe_L9 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L1 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L2 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L3 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L4 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L5 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L6 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L7 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L8 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY unc_Fe_L9 Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 ACE : ACE : ULEIS : ULEIS : HOURLY up_time_fraction Instrument team contact: Dennis Haggerty Phone: 240-228-7886 Org: John Hopkins University Applied Physics Laboratory Email: dennis.haggerty@jhuapl.edu Principal Investigator: Glenn Mason Phone: 240-228-2805 Org: JHU/Applied Physics Lab Email: Glenn.Mason@jhuapl.edu 1 1998-02-19 12:00:00 2007-05-18 12:00:00 AMPTE : AMPTE-UK : TDIE : TDIE : TDFR ISen/0 The following is a list of tables and constants in this vidf TABLE 0: telemetry decom table TABLE 1: step 1 in computation of center energies in scan TABLE 2: takes cal set 1 data to number of steps in scan TABLE 3: takes cal set 2 data to spin period in seconds TABLE 4: maximim scan energy (used in computation of energies) TABLE 5: geometry factors (m**2-ster) CONST 1: maximum polar look angles of detectors CONST 2: mimimum polar look angles of detectors The center energy of a the scan step depends on the spin rate. This is due to the fact that the instrument returns a fixed number of samples within a fixed fraction of a spin period even if the sweep rate being varied. The expression used to get the center energies is CE(SS) = Em * exp (-[15 * Sp * SS]/[256 * tc * NS]) where SS is the scan step number NS is the total number of scan steps Em is the maximum energy = 20000 eV tc is the time constant = .0385 Sp is the spin period in milliseconds The following units can be derived from the VIDF tables. The format is to give the tables applied followed by the table operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1,2,3,4 0,4,13,3 eV Sweep 0 0 cnts/accum Cal Set 1 2 0 time constant Cal Set 2 3 0 spin per (msec) Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@bilbo.space.swri.edu 32 1984-09-13 01:20:03 1984-09-13 01:20:03 AMPTE : AMPTE-UK : TDIE : TDIE : TDFR ISEN/1 The following is a list of tables and constants in this vidf TABLE 0: telemetry decom table TABLE 1: step 1 in computation of center energies in scan TABLE 2: takes cal set 1 data to number of steps in scan TABLE 3: takes cal set 2 data to spin period in seconds TABLE 4: maximim scan energy (used in computation of energies) TABLE 5: geometry factors (m**2-ster) CONST 1: maximum polar look angles of detectors CONST 2: mimimum polar look angles of detectors The center energy of a the scan step depends on the spin rate. This is due to the fact that the instrument returns a fixed number of samples within a fixed fraction of a spin period even if the sweep rate being varied. The expression used to get the center energies is CE(SS) = Em * exp (-[15 * Sp * SS]/[256 * tc * NS]) where SS is the scan step number NS is the total number of scan steps Em is the maximum energy = 20000 eV tc is the time constant = .0385 Sp is the spin period in milliseconds The following units can be derived from the VIDF tables. The format is to give the tables applied followed by the table operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1,2,3,4 0,4,13,3 eV Sweep 0 0 cnts/accum Cal Set 1 2 0 time constant Cal Set 2 3 0 spin per (msec) Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@bilbo.space.swri.edu 32 1984-09-13 01:20:03 1984-09-13 01:20:03 AMPTE : AMPTE-UK : TDIE : TDIE : TDFR ISEN/2 The following is a list of tables and constants in this vidf TABLE 0: telemetry decom table TABLE 1: step 1 in computation of center energies in scan TABLE 2: takes cal set 1 data to number of steps in scan TABLE 3: takes cal set 2 data to spin period in seconds TABLE 4: maximim scan energy (used in computation of energies) TABLE 5: geometry factors (m**2-ster) CONST 1: maximum polar look angles of detectors CONST 2: mimimum polar look angles of detectors The center energy of a the scan step depends on the spin rate. This is due to the fact that the instrument returns a fixed number of samples within a fixed fraction of a spin period even if the sweep rate being varied. The expression used to get the center energies is CE(SS) = Em * exp (-[15 * Sp * SS]/[256 * tc * NS]) where SS is the scan step number NS is the total number of scan steps Em is the maximum energy = 20000 eV tc is the time constant = .0385 Sp is the spin period in milliseconds The following units can be derived from the VIDF tables. The format is to give the tables applied followed by the table operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1,2,3,4 0,4,13,3 eV Sweep 0 0 cnts/accum Cal Set 1 2 0 time constant Cal Set 2 3 0 spin per (msec) Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@bilbo.space.swri.edu 32 1984-09-13 01:20:03 1984-09-13 01:20:03 AMPTE : AMPTE-UK : TDIE : TDIE : TDFR ISEN/3 The following is a list of tables and constants in this vidf TABLE 0: telemetry decom table TABLE 1: step 1 in computation of center energies in scan TABLE 2: takes cal set 1 data to number of steps in scan TABLE 3: takes cal set 2 data to spin period in seconds TABLE 4: maximim scan energy (used in computation of energies) TABLE 5: geometry factors (m**2-ster) CONST 1: maximum polar look angles of detectors CONST 2: mimimum polar look angles of detectors The center energy of a the scan step depends on the spin rate. This is due to the fact that the instrument returns a fixed number of samples within a fixed fraction of a spin period even if the sweep rate being varied. The expression used to get the center energies is CE(SS) = Em * exp (-[15 * Sp * SS]/[256 * tc * NS]) where SS is the scan step number NS is the total number of scan steps Em is the maximum energy = 20000 eV tc is the time constant = .0385 Sp is the spin period in milliseconds The following units can be derived from the VIDF tables. The format is to give the tables applied followed by the table operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1,2,3,4 0,4,13,3 eV Sweep 0 0 cnts/accum Cal Set 1 2 0 time constant Cal Set 2 3 0 spin per (msec) Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@bilbo.space.swri.edu 32 1984-09-13 01:20:03 1984-09-13 01:20:03 ARIA : ARIA-1 : OAAR : OAAR : ARAA Elap/Time Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Tr/SlntRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Tr/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Tr/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA L/HorizRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA L/N-S/Rng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA L/E-W/Rng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA L/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA G/Alt Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA G/Lat Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA G/Long Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Vel/ER Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Vel/E-W Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Vel/N-S Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA Vel/Alt Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA F/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA F/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA LAS/SlntRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA LAS/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAA LAS/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:07:02 1992-03-03 02:07:02 ARIA : ARIA-1 : OAAR : OAAR : ARAB Elap/Time Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB E/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB E/Yaw Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB E/Roll Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB Roll/Rt Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB Gim/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB XGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB XGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB YGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB YGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB ZGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB ZGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C11 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C12 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C13 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C21 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C22 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C23 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C31 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C32 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARAB RM/C33 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:06:47 1992-03-03 02:06:47 ARIA : ARIA-1 : OAAR : OAAR : ARMB Magnetometer Roll 2 Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB Magnetometer Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Impulse Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Pitch Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Yaw-Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Gyro Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB Gyro Yaw Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Roll Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Pitch Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMB ACS Yaw Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMF Magnetometer Roll 1 Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Roll Nozzle HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : OAAR : OAAR : ARMF ACS Roll Nozzle Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Roll Nozzle HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : ENG : ARMC SPS Swept High Voltage Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Pitch/Yaw Nozzles HEX 2 ACS Gyro Roll HEX VIDF sensors 1 and 2 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : ENG : ARMC ACS Pitch/Yaw Nozzles Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Pitch/Yaw Nozzles HEX 2 ACS Gyro Roll HEX VIDF sensors 1 and 2 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : ENG : ARMC ACS Gyro Roll Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Pitch/Yaw Nozzles HEX 2 ACS Gyro Roll HEX VIDF sensors 1 and 2 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : ENG : ARMD +5 Volt Regulated Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 +5 Volt Regulated Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : SPS : AREF SPS Electron Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : SPS : ARES e- RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : SPS : ARIF SPS Ion Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : SPS : ARIS i+ RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-1 : SPS : SPS : ARPA ARIA/SPS/PA Pitch angles are stored in radians. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1992-03-03 02:01:51 1992-03-03 02:01:51 ARIA : ARIA-2 : OAAR : OAAR : ARAB Elap/Time Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB E/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB E/Yaw Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB E/Roll Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB Roll/Rt Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB Gim/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB XGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB XGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB YGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB YGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB ZGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB ZGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C11 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C12 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C13 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C21 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C22 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C23 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C31 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C32 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARAB RM/C33 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:15:59 1994-02-12 01:15:59 ARIA : ARIA-2 : OAAR : OAAR : ARMB Magnetometer Roll 2 Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB Magnetometer Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Impulse Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Pitch Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Yaw Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Gyro Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Gyro Yaw Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Roll Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Pitch Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMB ACS Yaw Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARME Thrust Acceleration Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Thrust Acceleration HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARME Lateral Acceleration Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Thrust Acceleration HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMF Magnetometer Roll 1 Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : OAAR : OAAR : ARMF ACS Nozzles Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA SPS +5 Volt Battery Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA ACS Tank Pressure Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA ACS Roll Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA ACS Discretes Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA ACS Battery Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA TM +28 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA TM +28 Volt Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp +28 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp +28 Volts Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp +15 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp -15 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp +/- 15 Volt Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Pyro +20 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Nose Cone Eject Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Langmuir Probe Deploy Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMA Exp Reentry Door Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMC SPS Swept High Voltage Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMC ACS Roll Pot Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMC ACS Gyro Roll Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMC Lateral Acceleration Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMD +5 Volt Regulated Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 +5 Volt Regulated Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : ENG : ARMG SPS Sync Pulse Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 SPS Sync Pulse Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : SPS : AREF SPS Electron Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : SPS : ARES e- RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : SPS : ARIF SPS Ion Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : SPS : ARIS i+ RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-2 : SPS : SPS : ARPA ARIA/SPS/PA Pitch angles are stored in radians. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1994-02-12 01:11:41 1994-02-12 01:11:41 ARIA : ARIA-3 : OAAR : OAAR : ARAA Elap/Time Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Tr/SlntRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Tr/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Tr/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA L/HorizRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA L/N-S/Rng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA L/E-W/Rng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA L/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA G/Alt Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA G/Lat Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA G/Long Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Vel/ER Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Vel/E-W Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Vel/N-S Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA Vel/Alt Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA F/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA F/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA LAS/SlntRng Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA LAS/Az Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARAA LAS/Elev Table 0 converts meters to kilometers, but is only relivant to sensors which include a distance measure (note that distances are neasured in meters). Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Slant Range from Tracker meters 1 Azimuth from Tracker degrees 2 Elevation from Tracker degrees 3 Horizontal Range from Launcher meters 4 North-South Range from Launcher meters 5 East-West Range from Launcher meters 6 Azimuth of Vehicle from Launcher degrees 7 Altitude of Vehicle meters 8 Latitude of Sub-Vehicle Point degrees 9 Longitude of Sub-Vehicle Point degrees 10 Earth Relative Velocity meters/second 11 East-West Component of Velocity meters/second 12 North-South Component of Velocity meters/second 13 Altitude Component of Velocity meters/second 14 Flight Elevation Angle degrees 15 Flight Azimuth Angle degrees 16 Slant Range from Look Angle Station meters 17 Azimuth from Look Angle Station degrees 18 Elevation from Look Angle Station degrees 19 Elapsed Time second Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:27:32 1995-02-02 03:27:32 ARIA : ARIA-3 : OAAR : OAAR : ARMB Magnetometer Roll 2 Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB Magnetometer Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Impulse Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Pitch Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Yaw Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Gyro Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Gyro Yaw Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Roll Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Pitch Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMB ACS Yaw Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARME Thrust Acceleration Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Thrust Acceleration HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMF Magnetometer Roll 1 Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : OAAR : OAAR : ARMF ACS Nozzles Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA SPS +5 Volt Battery Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA ACS Tank Pressure Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA ACS Roll Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA ACS Discretes Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA ACS Battery Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA TM +28 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA TM +28 Volt Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp +28 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp +28 Volts Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp +15 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp -15 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp +/- 15 Volt Current Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Pyro +20 Volts Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Nose Cone Eject Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Langmuir Probe Deploy Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMA Exp Reentry Door Squib Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS +5 Volt Battery Monitor HEX 2 ACS Tank Pressure HEX 2 ACS Regulated Pressure HEX 3 ACS Discretes HEX 4 ACS Battery Monitor HEX 5 TM +28 Volts HEX 6 TM +28 Volt Current HEX 7 Exp +28 Volts HEX 8 Exp +28 Volt Current HEX 9 Exp +15 Volts HEX 10 Exp -15 Volts HEX 11 Exp $+-$15 Volt Current HEX 12 Pyro +20 Volts HEX 13 Nose Cone Eject Squib HEX 14 Langmuir Probe Deploy Squib HEX 15 Exp Reentry Door Squib HEX VIDF sensors 1 through 16 really belong in a seperate VIDF since they are really information relating to the space vehicle. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMC SPS Swept High Voltage Monitor Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMC ACS Roll Pot Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMC ACS Gyro Roll Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMC Lateral Acceleration Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 SPS Swept High Voltage Monitor HEX 1 ACS Roll Pot HEX 2 ACS Gyro Roll HEX 3 Lateral Acceleration HEX VIDF sensors 1, 2, and 3 really belong in an O/A VIDF since they are really O/A information. They are included here due to a past definition. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMD +5 Volt Regulated Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 +5 Volt Regulated Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : ENG : ARMG SPS Sync Pulse Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 SPS Sync Pulse Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : SPS : AREF SPS Electron Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : SPS : ARES e- RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : SPS : ARIF SPS Ion Flyback RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : SPS : ARIS i+ RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: SPS efficiency table at each energy step TABLE 2: SPS geometric factor (cm**2-sec) for the detector TABLE 3: SPS resolution (dE/E) for the sensor TABLE 4: eV to erg conversion (erg/eV) TABLE 5: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,4 0,3 erg SWEEP 1 4 cnts/acc (Eff. Cor.) SWEEP 1 154 cnts/sec SWEEP 1,2,3 154,4,4 cnts/(cm**2-ster-s) SWEEP 1,2,3,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 1,2,3,4 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 1,2,3,0,0,4,4,5 154,4,4,4,4,4,4,3 sec**3/km**6 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 15 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-3 : SPS : SPS : ARPA ARIA/SPS/PA Pitch angles are stored in radians. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-02-02 03:26:56 1995-02-02 03:26:56 ARIA : ARIA-4 : OAAR : OAAR : ARAB Elap/Time Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB E/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB E/Yaw Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB E/Roll Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB Roll/Rt Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB Gim/Pitch Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB XGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB XGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB YGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB YGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB ZGyro/El Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB ZGyro/Az Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C11 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C12 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C13 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C21 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C22 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C23 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C31 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C32 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARAB RM/C33 Elapsed Time is measured in seconds. Roll Rate is determined in revolutions/second. All matrix elements are unitless numbers. The remainder of the sensors in this VIDF are in degrees. Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Euler Pitch degrees 1 Euler Yaw degrees 2 Euler Roll degrees 3 Roll Rate revolutions/second 4 Z Elevation degrees 5 Z Azimuth degrees 6 Y Elevation degrees 7 Y Azimuth degrees 8 X Elevation degrees 9 X Azimuth degrees 10 Gimbal Pitch degrees 11 Matrix Element C11 unitless 12 Matrix Element C12 unitless 13 Matrix Element C13 unitless 14 Matrix Element C21 unitless 15 Matrix Element C22 unitless 16 Matrix Element C23 unitless 17 Matrix Element C31 unitless 18 Matrix Element C32 unitless 19 Matrix Element C33 unitless 20 Elapsed Time seconds Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:07:23 1995-11-27 08:07:23 ARIA : ARIA-4 : OAAR : OAAR : ARMB Magnetometer Roll 2 Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB Magnetometer Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Impulse Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Pitch Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Yaw Null Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Gyro Pitch Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Gyro Yaw Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Roll Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Pitch Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMB ACS Yaw Rate Sensors included within this VIDF are: Sensor Sensor Name IDF units Number 0 Magnetometer Roll 2 HEX 1 Magnetometer Pitch HEX 2 ACS Impulse HEX 3 ACS Pitch Null HEX 4 ACS Yaw Null HEX 5 ACS Gyro Pitch HEX 6 ACS Gyro Yaw HEX 7 ACS Roll Rate HEX 8 ACS Pitch Rate HEX 9 ACS Yaw Rate HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARME Thrust Acceleration Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Thrust Acceleration HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMF Magnetometer Roll 1 Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ARIA : ARIA-4 : OAAR : OAAR : ARMF ACS Nozzles Monitor Sensors included within this VIDF are: Sensor Sensor Name VIDF units Number 0 Magnetometer Roll 1 HEX 1 ACS Nozzles Monitor HEX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1995-11-27 08:04:02 1995-11-27 08:04:02 ASTRID : ASTRID-1 : ASU : HK : HK MCP deflection voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK SSD deflection voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK MCP bias voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK MIO bias voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK MCP grid voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK SSD temperature ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK EMIL temperature ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK EMIL bias voltage ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK S-band TX sec +28V ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK S-band TX prim +28V ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK 400 MHz TX sec +28V ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK 400 MHz TX prim +28V ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : HK : HK Receiver +28V ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : MAGF : MAGF Bx ASTRID:ASTRID-1:ASU:ASU:MAGF This virtual consists of data from the magnetometer 1 mounted on Astrid-1. The x- and z-components of the magnetic field are measured, the y-component is simulated by a phase shift of 90 degrees of the x-component. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : MAGF : MAGF By (Bx delayed 90 degrees) ASTRID:ASTRID-1:ASU:ASU:MAGF This virtual consists of data from the magnetometer 1 mounted on Astrid-1. The x- and z-components of the magnetic field are measured, the y-component is simulated by a phase shift of 90 degrees of the x-component. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : MAGF : MAGF Bz ASTRID:ASTRID-1:ASU:ASU:MAGF This virtual consists of data from the magnetometer 1 mounted on Astrid-1. The x- and z-components of the magnetic field are measured, the y-component is simulated by a phase shift of 90 degrees of the x-component. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Alpha 1 ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Alpha 2 ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Beta 1 ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Beta 2 ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS EMIL sweep ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Sun angle ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : ASU : SS : SS Spin phase ASTRID:ASTRID-1:ASU:SS:SS This virtual consists of data from the IRF built sun sensor mounted on Astrid-1. The sun sensor uses a 2-dimensional array and a pinhole "camera" to image the position of the sun on the array. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-01-30 08:46:06 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Altitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA CGLat ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA CGLong ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Latitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Longitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA MLT ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA L-shell ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Eclipse status ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Vx ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Vy ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Vz ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Sun-X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Sun-Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEI Sun-Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEO X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEO Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA GEO Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA RA ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Declination ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Sun Angle ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA B-field Angle ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : OA : OA : OA Spin period ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 1 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 2 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 3 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 4 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 5 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Sector 6 ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Parallel ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Anti-parallel ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : EMIL : EMIL Perpendicular ASTRID:ASTRID-1:PAYLOAD:EMIL:EMIL This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 4 1995-02-02 12:09:19 1995-08-02 12:00:00 ASTRID : ASTRID-1 : PAYLOAD : MIO : MIO MIO-1 ASTRID:ASTRID-1:PAYLOAD:MIO:MIO This virtual consists of data from the two MIO photometers on Astrid-1. MIO-1 measures Lyman alpha and MIO-2 oxygen emissions. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : MIO : MIO MIO-2 ASTRID:ASTRID-1:PAYLOAD:MIO:MIO This virtual consists of data from the two MIO photometers on Astrid-1. MIO-1 measures Lyman alpha and MIO-2 oxygen emissions. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : MIO : MIO Latitude ASTRID:ASTRID-1:PAYLOAD:MIO:MIO This virtual consists of data from the two MIO photometers on Astrid-1. MIO-1 measures Lyman alpha and MIO-2 oxygen emissions. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : MIO : MIO Longitude ASTRID:ASTRID-1:PAYLOAD:MIO:MIO This virtual consists of data from the two MIO photometers on Astrid-1. MIO-1 measures Lyman alpha and MIO-2 oxygen emissions. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 0 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 1 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 2 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 3 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 4 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 5 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 6 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 7 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 8 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 9 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 10 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 11 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 12 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 13 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 14 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 15 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 16 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 17 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 18 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 19 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 20 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 21 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 22 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : MCP Sector 23 ASTRID:ASTRID-1:PAYLOAD:PIPPI:MCP This virtual consists of data from the PIPPI (Prelude In Planetary Particle Imaging) MCP neutral particle imager. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: constant needed in going to dist. fn TABLE 7: (center energies)**2 (ergs**2) TABLE 8: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-14 11:22:14 1995-02-28 06:18:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 0 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 1 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 2 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 3 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 4 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 5 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 6 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 7 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 8 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 9 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 10 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 11 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 12 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 13 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 14 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-1 : PAYLOAD : PIPPI : SSD Sector 15 ASTRID:ASTRID-1:PAYLOAD:PIPPI:SSD This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 8 1995-02-07 11:14:14 1995-02-28 09:52:52 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres1 msp (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres2 msp (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres3 msp (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres1 mee (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres2 mee (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : BRES Bres3 mee (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:BRES This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. These residuals were calculated at KTH by subtracting a model field from the total. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-01 12:00:00 1999-06-15 10:56:30 ASTRID : ASTRID-2 : EMMA : EMMA-B : EMAG B1gei (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:EMAG This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-07 12:00:00 1999-02-07 12:00:00 ASTRID : ASTRID-2 : EMMA : EMMA-B : EMAG B2gei (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:EMAG This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-07 12:00:00 1999-02-07 12:00:00 ASTRID : ASTRID-2 : EMMA : EMMA-B : EMAG B3gei (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:EMAG This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-07 12:00:00 1999-02-07 12:00:00 ASTRID : ASTRID-2 : EMMA : EMMA-B : EMAG Btot (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:EMAG This virtual consists of data from the three axis science magnetometer on Astrid-2. Coordinate system transforms were performed at KTH Stockholm. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-07 12:00:00 1999-02-07 12:00:00 ASTRID : ASTRID-2 : EMMA : EMMA-B : PANG B field angle (v1) ASTRID:ASTRID-2:EMMA:EMMA-B:PANG Table 0: moves decimal place over one Table 1: 180 deg offset for spin axis units Table 2: 90 deg offset of spin plane units Unit 0: B/spin plane angle = data/10 - 90 Unit 1: B/spin axis angle = 180 - data/10 Wayne Keith Southwest Research Institute 6220 Culebra Rd. Div. 15 San Antonio, TX 78235 waynek@swri.edu 1 1999-02-07 12:00:00 1999-02-07 12:00:00 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1msp Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2msp Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3msp Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1mspp Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2mspp Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3mspp Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1mspr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2mspr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3mspr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1msppr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2msppr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3msppr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1meez Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2meez Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3meez Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1meep Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2meep Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3meep Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1meezr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2meezr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3meezr Eaxial=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 1meepr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 2meepr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : EFIELD E field 3meepr Eparallel=0 (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:EFIELD Electric field derived by KTH Stockholm from the EMMA electric field probes using various assumptions and coordinate systems. Spin plane components (msp coordinates) E1: 2x3 E2: in the spin plane perpendicular to B E3: along the spin axis z = spin axis component set to zero p = spin axis component caculated from Eparallel = 0 r = co-rotating frame E1mspz Eaxial=0, inertial frame E2mspz Eaxial=0, inertial frame E3mspz Eaxial=0, inertial frame (0 by def) E1mspp Eparallel=0, inertial frame ( = E1msp ) E2mspp Eparallel=0, inertial frame ( = E2msp ) E3mspp Eparallel=0, inertial frame E1mspr Eaxial=0, co-rotating frame E2mspr Eaxial=0, co-rotating frame E3mspr Eaxial=0, co-rotating frame (0 by def) E1msppr Eparallel=0, co-rotating frame ( = E1mspr ) E2msppr Eparallel=0, co-rotating frame ( = E2mspr ) E3msppr Eparallel=0, co-rotating frame Magnetic coordinate system (mee coordinates) E1: along B E2: perpendicular to B towards magnetic East E3: 1x2 (Equatorward) z, p, and r = same as above E1meez Eaxial=0, inertial frame E2meez Eaxial=0, inertial frame E3meez Eaxial=0, inertial frame E1meep Eparallel=0, inertial frame E2meep Eparallel=0, inertial frame E3meep Eparallel=0, inertial frame E1meezr Eaxial=0, co-rotating frame E2meezr Eaxial=0, co-rotating frame E3meezr Eaxial=0, co-rotating frame E1meepr Eparallel=0, co-rotating frame E2meepr Eparallel=0, co-rotating frame E3meepr Eparallel=0, co-rotating frame Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-01-31 11:59:59 1999-06-12 11:23:33 ASTRID : ASTRID-2 : EMMA : EMMA-E : SCPOT Spacecraft Potential (v1) ASTRID:ASTRID-2:EMMA:EMMA-E:SCPOT Satelite potential derived by KTH Stockholm from the EMMA electric field probes. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 256 1999-02-06 11:59:59 1999-02-07 10:54:31 ASTRID : ASTRID-2 : LINDA : LINDA : AC AC P1 ASTRID:ASTRID-2:LINDA:LINDA:AC A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 2: BIAS VOLTAGE TABLE 3: BIT RESOLUTION, 8, 10 or 12 bits per data The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 16 1998-12-14 12:08:55 1999-07-24 07:50:06 ASTRID : ASTRID-2 : LINDA : LINDA : AC AC P2 ASTRID:ASTRID-2:LINDA:LINDA:AC A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 2: BIAS VOLTAGE TABLE 3: BIT RESOLUTION, 8, 10 or 12 bits per data The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 16 1998-12-14 12:08:55 1999-07-24 07:50:06 ASTRID : ASTRID-2 : LINDA : LINDA : DC DC P1 ASTRID:ASTRID-2:LINDA:LINDA:DC A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 2: BIAS VOLTABE TABLE 3: uni or bipolar mode The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 60 1998-12-14 12:08:55 1999-07-24 07:48:06 ASTRID : ASTRID-2 : LINDA : LINDA : DC DC P2 ASTRID:ASTRID-2:LINDA:LINDA:DC A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 2: BIAS VOLTABE TABLE 3: uni or bipolar mode The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 60 1998-12-14 12:08:55 1999-07-24 07:48:06 ASTRID : ASTRID-2 : LINDA : LINDA : SWEEP BiasInfo ASTRID:ASTRID-2:LINDA:LINDA:SWEEP A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 3: uni or bipolar mode The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 32 1998-12-14 12:09:55 1999-07-24 07:50:06 ASTRID : ASTRID-2 : LINDA : LINDA : SWEEP SWEEP P1 ASTRID:ASTRID-2:LINDA:LINDA:SWEEP A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 3: uni or bipolar mode The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 32 1998-12-14 12:09:55 1999-07-24 07:50:06 ASTRID : ASTRID-2 : LINDA : LINDA : SWEEP SWEEP P2 ASTRID:ASTRID-2:LINDA:LINDA:SWEEP A complete description of the instrument can be found in: The development of the scientific measuring instruments LINDA, a part of the payload on the Swedish micro-satellite Astrid-2 The following is a list of tables which are in this vidf TABLE 0: resistor value for pregain TABLE 1: pA unit TABLE 3: uni or bipolar mode The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT OLLE NORBERG Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Olle@irf.se 32 1998-12-14 12:09:55 1999-07-24 07:50:06 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 0 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 1 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 2 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 3 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 4 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 5 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 6 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 7 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 8 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 9 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 10 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 11 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 12 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 13 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 14 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 15 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 0 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 1 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 2 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 3 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 4 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 5 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 6 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 7 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 8 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 9 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 10 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 11 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 12 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 13 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 14 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 15 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1998-12-14 12:15:47 1999-07-24 06:52:05 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA PIA/PhotC ASTRID:ASTRID-2:MEDUSA:PIA:PIA This vidf contains SOMEINSTRUMENT data taken from Photometer 1. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-18 12:35:38 1998-12-18 12:35:38 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA PIA/C/Glong ASTRID:ASTRID-2:MEDUSA:PIA:PIA This vidf contains SOMEINSTRUMENT data taken from Photometer 1. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-18 12:35:38 1998-12-18 12:35:38 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA PIA/C/Glat ASTRID:ASTRID-2:MEDUSA:PIA:PIA This vidf contains SOMEINSTRUMENT data taken from Photometer 1. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-18 12:35:38 1998-12-18 12:35:38 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 1 pixel 0 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 1 pixel 1 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 1 pixel 2 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 1 pixel 3 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 2 pixel 0 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 2 pixel 1 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 2 pixel 2 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : MEDUSA : PIA : PIA1_2 PIA 2 pixel 3 TABLE 0: raw counts/accumulation David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 64 1998-12-21 01:24:58 1999-07-24 10:08:42 ASTRID : ASTRID-2 : OA : OA : OA Altitude ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA CGLat ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA CGLong ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Latitude ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Longitude ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA MLT ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA L-shell ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Eclipse status ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI X ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Y ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Z ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Vx ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Vy ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Vz ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Sun-X ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Sun-Y ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEI Sun-Z ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEO X ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEO Y ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA GEO Z ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA RA ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Declination ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Sun Angle ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA B-field Angle ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2 : OA : OA : OA Satellite Time Word ASTRID:ASTRID-2:OA:OA:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1998-12-11 03:43:38 1999-07-24 10:54:41 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 0 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 1 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 2 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 3 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 4 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 5 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 6 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 7 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 8 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 9 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 10 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 11 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 12 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 13 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 14 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSE Astrid-2 MEDUSA Electron -sector 15 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 0 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 1 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 2 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 3 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 4 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 5 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 6 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 7 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 8 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 9 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 10 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 11 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 12 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 13 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 14 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : MDSI Astrid-2 MEDUSA Ion -sector 15 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-18 08:53:32 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E Astrid-2 MEDUSA Electron -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_E_C MEDUSA corrected Electron -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 4 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I Astrid-2 MEDUSA Ion -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Parallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Perpendicular The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 ASTRID : ASTRID-2-SANAE : MEDUSA : MEDUSA : SEL_I_C Astrid-2 corrected MEDUSA Ion -Antiparallel The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,5 0,154,4,4,3 ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 1999-02-13 08:15:31 1999-07-24 06:52:05 CUSP : PFAFF : CED : CED : CEDS CED -sector 0 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 1 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 2 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 3 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 4 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 5 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 6 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 7 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 8 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 9 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 10 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 11 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 12 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 13 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 14 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 15 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 16 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 17 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 18 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 19 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 20 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 21 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 22 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CED : CED : CEDS CED -sector 23 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: SPS efficiency table at each energy step TABLE 3: SPS geometric factor (cm**2-sec) for the detector TABLE 4: SPS resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 0 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 1 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 2 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 3 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 4 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 5 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 6 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 7 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 8 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 9 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 10 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 11 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 12 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 13 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 14 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 15 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 16 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 17 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 18 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 19 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 20 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 21 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 22 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : CID : CID : CIDS CID -sector 23 RAW units stored in the IDF file are the integer counts. In order to convert to various units, tables are applied and are defined below. The following is a list of tables included in this VIDF: TABLE 0: table of center energies (eV) of each energy step TABLE 1: telemetry decompression table TABLE 2: CID efficiency table at each energy step TABLE 3: CID geometric factor (cm**2-sec) for the detector TABLE 4: CID resolution (dE/E) for the sensor TABLE 5: eV to erg conversion (erg/eV) TABLE 6: conversion to distribution function The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,5 0,3 erg SWEEP 1 0 cnts SWEEP 2 4 cnts/acc (Eff. Cor.) SWEEP 2 154 cnts/sec SWEEP 2,3,4 154,4,4 cnts/(cm**2-ster-s) SWEEP 2,3,4,0 154,4,4,4 cnts/(cm**2-ster-s-eV) SWEEP 2,3,4,5 154,4,4,3 ergs/(cm**2-ster-s-eV) SWEEP 2,3,4,0,0,5,5,6 154,4,4,4,4,4,4,3 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238 1 1997-12-03 09:05:59 1997-12-03 09:05:59 CUSP : PFAFF : MAG : ASP_MAG : AAMG Aspect Bx This virtual contains aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:05:01 1997-12-03 09:05:01 CUSP : PFAFF : MAG : ASP_MAG : AAMG Aspect By This virtual contains aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:05:01 1997-12-03 09:05:01 CUSP : PFAFF : MAG : ASP_MAG : AAMG Aspect Bz This virtual contains aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:05:01 1997-12-03 09:05:01 CUSP : PFAFF : OA : OA : AAOA Flight Time This virtual contains computed OA (flt time,alt,lat,lon) data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:06:00 1997-12-03 09:06:00 CUSP : PFAFF : OA : OA : AAOA Altitude This virtual contains computed OA (flt time,alt,lat,lon) data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:06:00 1997-12-03 09:06:00 CUSP : PFAFF : OA : OA : AAOA Latitude This virtual contains computed OA (flt time,alt,lat,lon) data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:06:00 1997-12-03 09:06:00 CUSP : PFAFF : OA : OA : AAOA Longitude This virtual contains computed OA (flt time,alt,lat,lon) data. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 jsharber@swri.edu 1 1997-12-03 09:06:00 1997-12-03 09:06:00 DE : DE-1 : HAPI : HAPI : D1HE e- Sen 0 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: electron mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Electrons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HE e- Sen 2 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: electron mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Electrons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HE e- Sen 4 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: electron mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Electrons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HI p+ Sen 1 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: proton mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Protons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HI p+ Sen 3 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: proton mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Protons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HI p+ Sen 5 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: proton mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Protons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HI p+ Sen 7 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: proton mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Protons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : HAPI : HAPI : D1HI p+ Sen 9 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal(s) to the HAPI detector aperatures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction of the field vector, i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: High-Altitude Plasma Instrument for Dybamics Explorer-A Burch, J. L. et al. Space Science Instrumentation, V5, pp 455-464, 1981. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: energy resolution (dE/E) TABLE 5: center energies (ergs) TABLE 6: conversion factor from eV to ergs TABLE 7: (center energies)**2 (ergs**2) TABLE 8: constant needed in going to dist. fn TABLE 9: conversion factor from eV to Joule TABLE 10: proton mass in kg TABLE 11: number 2 TABLE 12: conversion factor from m to km TABLE 13: conversion factor from m***6 to km**6 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV (center) Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6 0,154,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,8 0,154,4,4,4,3 sec**3/km**6 Sweep 1,2,3,4,7,8. 0,154,4,4,4,3. sec**3/m**6 13 4 Scan 0,9,11,10 0,3,3,64 m/s (center) Scan 0,9,11,10,12 0,3,3,64,4 km/s (center) Dr. Jim Burch Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 DE-1 Protons Measured by HAPI 4 1981-09-02 05:29:22 1981-12-01 07:14:09 DE : DE-1 : OA : OA : D1OA Period This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Inclin This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Eccen This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SemiMaj This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA ArgOfPrge This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA RA AscNode This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI NV/P This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI NV/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI NV/V This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Apogee This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Perigee This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Orbit # This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TmFmPrge This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Lit/Drk This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GrnwST This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISUN/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISUN/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISUN/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEIMOON/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEIMOON/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEIMOON/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISPOS/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISPOS/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISPOS/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVEL/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVEL/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVEL/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVRRA/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVRRA/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISVRRA/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA AltOvSph This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GeodLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GcenLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GmagLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA ELong This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA MinRayH This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA MimRayLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA LASTm This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA LMTm This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA LShell This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA IL This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TotB This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI/Bx This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI/By This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEI/Bz This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Br This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Bt This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA Bp This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GcenMagI This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEINIngr/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEINIngr/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEINIngr/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISEgr/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISEgr/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISEgr/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA NIngr/Lat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA NIngr/Long This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SEgr/Lat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SEgr/Long This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A11 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A21 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A31 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A12 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A22 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A32 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A13 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A23 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA TMat/A33 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISatL/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISatL/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA GEISatL/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SpinAng This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SpinRate This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA ConingAng This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA ConingRate This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA ConingPha This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : OA : OA : D1OA SZA This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-1 Spacecraft 1 1981-08-15 12:00:00 1982-01-01 10:00:00 DE : DE-1 : PWI : PWI : PWILF Ant-A/EF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWILF This virtual contains the low frequency measurements (linear portion) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu Low Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWILF Ant-A/MF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWILF This virtual contains the low frequency measurements (linear portion) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu Low Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWILF Ant-B/EF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWILF This virtual contains the low frequency measurements (linear portion) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu Low Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWILF Ant-B/MF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWILF This virtual contains the low frequency measurements (linear portion) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu Low Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWISF Ant-A/EF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWISF This virtual contains the high frequency measurements ( >100 Hz) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu High Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWISF Ant-A/MF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWISF This virtual contains the high frequency measurements ( >100 Hz) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu High Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWISF Ant-B/EF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWISF This virtual contains the high frequency measurements ( >100 Hz) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu High Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : PWI : PWI : PWISF Ant-B/MF DATA SOURCE: DE-1 DE:DE-1:PWI:PWI:PWISF This virtual contains the high frequency measurements ( >100 Hz) of the electric / magnetic plasma waves. The following is a list of tables which are in this vidf TABLE 0: Table of center frequencies (Hz) TABLE 1: Table of center frequencies (kHz) The following shows the units of the sensors and also the units which can be constructed from the included tables. DATA TYPE SEN TABLES OPERS UNIT Sweep - - - volts**2/(m**2-Hz) Scan all 0 0 Hz Scan all 1 0 kHz Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swri.edu High Frequency DE-1 Plasma Electric and Magnetic Waves 1 1981-09-16 05:20:12 1981-11-27 04:34:54 DE : DE-1 : SAI : SAI : SAIA SAI/PhotA This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer A Images from the DE-1 Spacecraft 20 1981-10-17 12:56:26 1981-11-17 05:28:42 DE : DE-1 : SAI : SAI : SAIA SAI/A/Glong This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer A Images from the DE-1 Spacecraft 20 1981-10-17 12:56:26 1981-11-17 05:28:42 DE : DE-1 : SAI : SAI : SAIA SAI/A/Glat This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer A Images from the DE-1 Spacecraft 20 1981-10-17 12:56:26 1981-11-17 05:28:42 DE : DE-1 : SAI : SAI : SAIB SAI/PhotB This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer B Images from the DE-1 Spacecraft 20 1981-10-17 12:56:22 1981-11-17 05:28:44 DE : DE-1 : SAI : SAI : SAIB SAI/B/Glong This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer B Images from the DE-1 Spacecraft 20 1981-10-17 12:56:22 1981-11-17 05:28:44 DE : DE-1 : SAI : SAI : SAIB SAI/B/Glat This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer B Images from the DE-1 Spacecraft 20 1981-10-17 12:56:22 1981-11-17 05:28:44 DE : DE-1 : SAI : SAI : SAIC SAI/PhotC This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer C Images from the DE-1 Spacecraft 20 1981-09-24 12:04:31 1981-11-17 05:30:58 DE : DE-1 : SAI : SAI : SAIC SAI/C/Glong This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer C Images from the DE-1 Spacecraft 20 1981-09-24 12:04:31 1981-11-17 05:30:58 DE : DE-1 : SAI : SAI : SAIC SAI/C/Glat This vidf contains SAI imaging data taken from Photometer A. Original problems with ric-rac patterns in the images were corrected by disabling the nadar corrections in UofIowa code giving geographic coordinates. Conversion to kR now works by using the ascii filter name given in data header to obtain the the conversion factors rather than the analog filter wheel position which seem to give positions not pointing to any of the filter positions. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to counts per accumulation period for sensor 0 and longitude and latitude for sensors 1 and 2 respectively TABLE 1: Conversion of photometer data to kilorayleighs TABLE 2: Telemetry to pixels for cal set 1 TABLE 3: Telemetry to pixels for cal set 2 TABLE 4: Telemetry to pixels for cal set 3 TABLE 5: Telemetry to degrees C for cal set 6 TABLE 6: ascii definitions for some status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 cnts/accum Sensor 0 0 1 0 4 kilorayleigh Sensor 1,2 0 0 deg Scan 2 3 4 1 1 1 cor. pixels Cal 1 2 0 pixels Cal 2 3 0 pixels Cal 3 4 0 pixels Cal 6 5 0 degrees C Chris Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 chris@pemrac.space.swi.edu Photometer C Images from the DE-1 Spacecraft 20 1981-09-24 12:04:31 1981-11-17 05:30:58 DE : DE-2 : FPI : FPI : DFPI WindSpeed This virtual contains the Fabry-Perot interferometer data from the DE-2 satellite. The experiment is described in: The Fabry-Perot Interferometer on Dynamics Explorer Hays, P.B. et al. Space Science Instrumentation, V5, pp 395-416, 1991 The units of the returned data are as follows SENSORS UNITS 0 m/s 1 degrees K 2 dimensionless Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Fabry-Perot data (Wind Speed, Neutral Temperature, Brightness) 1 1981-11-01 11:42:00 1983-01-30 06:43:52 DE : DE-2 : FPI : FPI : DFPI Temp This virtual contains the Fabry-Perot interferometer data from the DE-2 satellite. The experiment is described in: The Fabry-Perot Interferometer on Dynamics Explorer Hays, P.B. et al. Space Science Instrumentation, V5, pp 395-416, 1991 The units of the returned data are as follows SENSORS UNITS 0 m/s 1 degrees K 2 dimensionless Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Fabry-Perot data (Wind Speed, Neutral Temperature, Brightness) 1 1981-11-01 11:42:00 1983-01-30 06:43:52 DE : DE-2 : FPI : FPI : DFPI Brightness This virtual contains the Fabry-Perot interferometer data from the DE-2 satellite. The experiment is described in: The Fabry-Perot Interferometer on Dynamics Explorer Hays, P.B. et al. Space Science Instrumentation, V5, pp 395-416, 1991 The units of the returned data are as follows SENSORS UNITS 0 m/s 1 degrees K 2 dimensionless Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Fabry-Perot data (Wind Speed, Neutral Temperature, Brightness) 1 1981-11-01 11:42:00 1983-01-30 06:43:52 DE : DE-2 : LANG : LANG : LANG e- Temp This virtual instrument contains the electron temperature and density at the DE-2 satellite as well as the ion density and the satellite potential. All quantities are obtained by reduction of Langmuir probe data. A complete description of this instrument is found in: The Dynamics Explorer Langmuir Probe Instrument Krehbiel, J. P. et al. Space Science Instrumentation, V5, pp 493-502, 1981 The units of the returned data are as follows SENSORS UNITS 0-2 #/cc 3 volts David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu DE-2 Langmuir Probe Elec. Temperature, Density, Spacecraft Potential 1 1981-08-05 01:25:02 1982-09-06 10:22:52 DE : DE-2 : LANG : LANG : LANG e- Den This virtual instrument contains the electron temperature and density at the DE-2 satellite as well as the ion density and the satellite potential. All quantities are obtained by reduction of Langmuir probe data. A complete description of this instrument is found in: The Dynamics Explorer Langmuir Probe Instrument Krehbiel, J. P. et al. Space Science Instrumentation, V5, pp 493-502, 1981 The units of the returned data are as follows SENSORS UNITS 0-2 #/cc 3 volts David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu DE-2 Langmuir Probe Elec. Temperature, Density, Spacecraft Potential 1 1981-08-05 01:25:02 1982-09-06 10:22:52 DE : DE-2 : LANG : LANG : LANG i+ Den This virtual instrument contains the electron temperature and density at the DE-2 satellite as well as the ion density and the satellite potential. All quantities are obtained by reduction of Langmuir probe data. A complete description of this instrument is found in: The Dynamics Explorer Langmuir Probe Instrument Krehbiel, J. P. et al. Space Science Instrumentation, V5, pp 493-502, 1981 The units of the returned data are as follows SENSORS UNITS 0-2 #/cc 3 volts David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu DE-2 Langmuir Probe Elec. Temperature, Density, Spacecraft Potential 1 1981-08-05 01:25:02 1982-09-06 10:22:52 DE : DE-2 : LANG : LANG : LANG sc pot This virtual instrument contains the electron temperature and density at the DE-2 satellite as well as the ion density and the satellite potential. All quantities are obtained by reduction of Langmuir probe data. A complete description of this instrument is found in: The Dynamics Explorer Langmuir Probe Instrument Krehbiel, J. P. et al. Space Science Instrumentation, V5, pp 493-502, 1981 The units of the returned data are as follows SENSORS UNITS 0-2 #/cc 3 volts David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu DE-2 Langmuir Probe Elec. Temperature, Density, Spacecraft Potential 1 1981-08-05 01:25:02 1982-09-06 10:22:52 DE : DE-2 : LAPI : LAPI : D2GMT 0 deg Geiger Tube DE:DE-1:LAPI:LAPI:D2LE This virtual contains the geiger tube data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table (counts/accum) TABLE 1: geometry factors (cm**2-str) The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Sen 0 0 cnts/accum Sen 0 150 cnts/sec Sen 0,1 150,4 cnts/(cm**2-str-s) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 High Energy Particles Measured by LAPI Giger Tubes 32 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2GMT 90 deg Geiger Tube DE:DE-1:LAPI:LAPI:D2LE This virtual contains the geiger tube data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table (counts/accum) TABLE 1: geometry factors (cm**2-str) The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Sen 0 0 cnts/accum Sen 0 150 cnts/sec Sen 0,1 150,4 cnts/(cm**2-str-s) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 High Energy Particles Measured by LAPI Giger Tubes 32 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (0+ deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (-180 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (30 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (172 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (7.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (45 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (112.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (97.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (165 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (60 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (135.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (105 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (15 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (+180 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (-0 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (0+ deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (-180 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (30 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (172 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (7.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (45 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (112.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (97.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (165 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (60 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (135.5 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (105 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (15 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (+180 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LE e- (-0 deg) DE:DE-1:LAPI:LAPI:D2LE This virtual contains the electron sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: electron mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Electrons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (0+ deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (-180 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (30 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (172 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (7.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (45 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (112.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (97.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (165 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (60 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (135.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (105 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (15 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (+180 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (-0 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (0+ deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (-180 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (30 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (172 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (7.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (45 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (112.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (97.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (165 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (60 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (135.5 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (105 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (15 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (+180 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : LAPI : LAPI : D2LI p+ (-0 deg) DE:DE-1:LAPI:LAPI:D2LI This virtual contains the ion sensor data from the Dynamics Explorer - 2 Low Altitude Plasma Instrument. The following should be noted: All of the rotation angles are determined from the scan platform position. Likewise, the spin rate is the rotation rate of the scan platform. Much time there is no spin rate and the sun-sensor crossing holds the current scan platform angle (see IDFS definition). When the scan platform is in motion, the motion is generally slow, derived from movement tracking the magntic field. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table (counts/accum) TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: 2 count threshold table TABLE 8: conversion factor from eV to Joule TABLE 9: proton mass in kg TABLE 10: number 2 TABLE 11: conversion factor from m to km TABLE 12: conversion factor from m***6 to km**6 CONST 1: maximum polar angles of detectors CONST 2: minimum polar angles of detectors The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Sen 1,2,3,4,6,5,0,5,0, 0,153,4,4,3,4,4,4,4, sec**3/m**6 12 4 Scan 0,8 0,3 Joule Scan 0,8,10,9 0,3,3,64 m/s Scan 0,8,10,9,11 0,3,3,64,4 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Protons Measured by LAPI 4 1981-08-16 05:56:06 1983-02-07 06:28:42 DE : DE-2 : MAGB : MAGB : MAGB Sat/Bx This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/By This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/Bz This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Bsline/Bx This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Bsline/By This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Bsline/Bz This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/Mod/Bx This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/Mod/By This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/Mod/Bz This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/dBx This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/dBy This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB Sat/dBz This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Br This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Bt This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Bp This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Mod/Br This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Mod/Bt This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/Mod/Bp This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/dBr This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/dBt This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB GGS/dBp This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB dB_para This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB dB_NS This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : MAGB : MAGB : MAGB dB_EW This virtual instrument contains both measured and derived quantities from the magnetometer on board DE-2. All data is as integers * 10**4. A complete description of this instrument is found in: Magnetic Field Observations on DE-A and DE-B Farthing, W. H. et al. Space Science Instrumentation, V5, pp 551-560, 1981 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the 10**4 multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA SEN TABLES OPERS UNIT Sweep all 0 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu Earth's Magnetic Field for the DE-2 Spacecraft 1 1981-08-15 05:56:28 1981-12-31 05:37:41 DE : DE-2 : NACS : NACS : NACS N2 Density This virtual contains the neutral atmosphere composition data from the DE-2 satellite. The experiment is described in: The Neutral Mass Spectrometer On Dynamics Explorer B Carigan, G.R. et al. Space Science Instrumentation, V5, pp 429-441, 1991 The units of the returned data are as follows SENSORS UNITS 0-4 #/cc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Neutral Atmosphere Composition Data (N2, O, He, Ar, N) 1 1981-11-01 12:00:08 1983-01-31 02:13:44 DE : DE-2 : NACS : NACS : NACS O Density This virtual contains the neutral atmosphere composition data from the DE-2 satellite. The experiment is described in: The Neutral Mass Spectrometer On Dynamics Explorer B Carigan, G.R. et al. Space Science Instrumentation, V5, pp 429-441, 1991 The units of the returned data are as follows SENSORS UNITS 0-4 #/cc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Neutral Atmosphere Composition Data (N2, O, He, Ar, N) 1 1981-11-01 12:00:08 1983-01-31 02:13:44 DE : DE-2 : NACS : NACS : NACS He Density This virtual contains the neutral atmosphere composition data from the DE-2 satellite. The experiment is described in: The Neutral Mass Spectrometer On Dynamics Explorer B Carigan, G.R. et al. Space Science Instrumentation, V5, pp 429-441, 1991 The units of the returned data are as follows SENSORS UNITS 0-4 #/cc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Neutral Atmosphere Composition Data (N2, O, He, Ar, N) 1 1981-11-01 12:00:08 1983-01-31 02:13:44 DE : DE-2 : NACS : NACS : NACS Ar Density This virtual contains the neutral atmosphere composition data from the DE-2 satellite. The experiment is described in: The Neutral Mass Spectrometer On Dynamics Explorer B Carigan, G.R. et al. Space Science Instrumentation, V5, pp 429-441, 1991 The units of the returned data are as follows SENSORS UNITS 0-4 #/cc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Neutral Atmosphere Composition Data (N2, O, He, Ar, N) 1 1981-11-01 12:00:08 1983-01-31 02:13:44 DE : DE-2 : NACS : NACS : NACS N Density This virtual contains the neutral atmosphere composition data from the DE-2 satellite. The experiment is described in: The Neutral Mass Spectrometer On Dynamics Explorer B Carigan, G.R. et al. Space Science Instrumentation, V5, pp 429-441, 1991 The units of the returned data are as follows SENSORS UNITS 0-4 #/cc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 Neutral Atmosphere Composition Data (N2, O, He, Ar, N) 1 1981-11-01 12:00:08 1983-01-31 02:13:44 DE : DE-2 : OA : OA : D2OA Period This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Inclin This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Eccen This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SemiMaj This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA ArgOfPrge This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA RA AscNode This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI NV/P This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI NV/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI NV/V This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Apogee This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Perigee This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Orbit # This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TmFmPrge This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Lit/Drk This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GrnwST This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISUN/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISUN/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISUN/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEIMOON/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEIMOON/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEIMOON/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISPOS/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISPOS/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISPOS/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVEL/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVEL/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVEL/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVRRA/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVRRA/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISVRRA/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA AltOvSph This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GeodLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GcenLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GmagLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA ELong This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA MinRayH This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA MimRayLat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA LASTm This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA LMTm This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA LShell This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA IL This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TotB This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI/Bx This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI/By This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEI/Bz This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Br This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Bt This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA Bp This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GcenMagI This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEINIngr/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEINIngr/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEINIngr/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISEgr/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISEgr/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISEgr/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA NIngr/Lat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA NIngr/Long This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SEgr/Lat This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SEgr/Long This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A11 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A21 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A31 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A12 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A22 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A32 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A13 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A23 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA TMat/A33 This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISatL/X This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISatL/Y This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA GEISatL/Z This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SpinAng This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SpinRate This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA ConingAng This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA ConingRate This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA ConingPha This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : OA : OA : D2OA SZA This virtual instrument contains the orbit/attitude data for DE-1 which was obtained from a NASA Goddard supplied algorithm and data file. The algorithm returns specified data values over a given time range with an arbitrary temporal resolution input by the user. All data in this file are given on 10 sec boundaries. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table removing the data multipliers The units of the returned data are as follows: SENSORS UNITS ----------- -------- 0 minutes 1, 4, 5, 31-34, 36, 40, 48, 55-58, 71, 73-76 degrees 2, 6-8, 11, 13, 39, 59-70 unitless 3, 9, 10, 18-23, 30, 35, 49-54 kilometers 12, 72 seconds 14 radians 15-17 AU 24-29 km/sec 37-38 hours 41-47 gauss David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu Orbit and Attitude Parameters for the DE-2 Spacecraft 1 1981-08-15 12:00:00 1981-12-27 10:00:00 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/Ax This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/Ay This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/Az This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/Bx This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/By This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACAB VEFI/AC/Bz This virtual contains the AC Electric Field Measurements from VEFI Spectrometer A and B. At each time, there is one output from each Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer A and B 32 1981-08-10 06:29:49 1982-11-30 08:02:24 DE : DE-2 : VEFI : AC : VACC VEFI/AC/Cx This virtual contains the AC Electric Field Measurements from VEFI Spectrometer C. At each time, there is one output from eacj Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer C 32 1981-08-10 06:29:49 1982-11-30 08:34:16 DE : DE-2 : VEFI : AC : VACC VEFI/AC/Cy This virtual contains the AC Electric Field Measurements from VEFI Spectrometer C. At each time, there is one output from eacj Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer C 32 1981-08-10 06:29:49 1982-11-30 08:34:16 DE : DE-2 : VEFI : AC : VACC VEFI/AC/Cz This virtual contains the AC Electric Field Measurements from VEFI Spectrometer C. At each time, there is one output from eacj Spectrometer and each Spectrometer may be connected to either the X, Y, or Z antenna. Data from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 AC Electric Field from VEFI Spectrometer C 32 1981-08-10 06:29:49 1982-11-30 08:34:16 DE : DE-2 : VEFI : DC : VEFIDC VEFI/DC/Ex This virtual contains the DC Electric Field Measurements from VEFI. Data is stored as floating point values of Volts/m. VEFI is composed of three antenna and the Z antenna failed to deploy. Thus, data measurements from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 DC Electric Field from VEFI 1 1981-08-17 05:26:54 1983-02-15 01:54:12 DE : DE-2 : VEFI : DC : VEFIDC VEFI/DC/Ey This virtual contains the DC Electric Field Measurements from VEFI. Data is stored as floating point values of Volts/m. VEFI is composed of three antenna and the Z antenna failed to deploy. Thus, data measurements from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 DC Electric Field from VEFI 1 1981-08-17 05:26:54 1983-02-15 01:54:12 DE : DE-2 : VEFI : DC : VEFIDC VEFI/DC/Ez This virtual contains the DC Electric Field Measurements from VEFI. Data is stored as floating point values of Volts/m. VEFI is composed of three antenna and the Z antenna failed to deploy. Thus, data measurements from the Z component are not correct and do not resemble any known voltage. The Z component values should be ignored. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu DE-2 DC Electric Field from VEFI 1 1981-08-17 05:26:54 1983-02-15 01:54:12 DE : DE-2 : WATS : WATS : WATS HorWindSpd This virtual contains the neutral wind and temperature data from the DE-2 satellite. The experiment is described in: The Dynamics Explorer Wind and Temperature Spectrometer Spencer, N.W. et al. Space Science Instrumentation, V5, pp 417-428, 1991 The units of the returned data are as follows SENSORS UNITS 0-1 m/s 2 degrees K Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 DC Neutral Wind and Temperature Data 1 1981-11-01 11:35:44 1983-01-31 10:48:32 DE : DE-2 : WATS : WATS : WATS VerWindSpd This virtual contains the neutral wind and temperature data from the DE-2 satellite. The experiment is described in: The Dynamics Explorer Wind and Temperature Spectrometer Spencer, N.W. et al. Space Science Instrumentation, V5, pp 417-428, 1991 The units of the returned data are as follows SENSORS UNITS 0-1 m/s 2 degrees K Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 DC Neutral Wind and Temperature Data 1 1981-11-01 11:35:44 1983-01-31 10:48:32 DE : DE-2 : WATS : WATS : WATS Temp This virtual contains the neutral wind and temperature data from the DE-2 satellite. The experiment is described in: The Dynamics Explorer Wind and Temperature Spectrometer Spencer, N.W. et al. Space Science Instrumentation, V5, pp 417-428, 1991 The units of the returned data are as follows SENSORS UNITS 0-1 m/s 2 degrees K Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78238-5166 david@dews1.space.swri.edu DE-2 DC Neutral Wind and Temperature Data 1 1981-11-01 11:35:44 1983-01-31 10:48:32 DMSP : DMSP-F06 : OA : OA : 06OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : OA : OA : 06OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F06 Orbit Data 15 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : SSJ4 : SSJ4 : 06SE High Energy SSJ/4 Electrons New VIDF cloned from 08SE Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F06 High and Low Energy SSJ/4 Electrons 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : SSJ4 : SSJ4 : 06SE Low Energy SSJ/4 Electrons New VIDF cloned from 08SE Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F06 High and Low Energy SSJ/4 Electrons 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : SSJ4 : SSJ4 : 06SI High Energy SSJ/4 Protons New VIDF cloned from 09SI Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F06 High and Low Energy SSJ/4 Protons 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F06 : SSJ4 : SSJ4 : 06SI Low Energy SSJ/4 Protons New VIDF cloned from 09SI Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F06 High and Low Energy SSJ/4 Protons 60 1983-12-01 12:22:03 1987-07-22 09:47:58 DMSP : DMSP-F07 : OA : OA : 07OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDFS units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) [not working] PACE model data are for the local (not mapped) magnetic position and co-rotate with the planet. They are similar to the standard MAG units except for the model used. One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geodetic and PACE Model Corrected DMSP-F06 Orbit Data 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : OA : OA : 07OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as fo Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Geomagnetic data are for the local (not mapped) magnetic position and co-rotate with the planet. They use the IGRF magnetic field model and are equivalent to MAG coordinates. Longitude has a range of +/- 180 deg. The L-shell value is figured from the equatorially-mapped field line altitude, and the invariant latitude is mapped to the nearest hemisphere's surface via the equation (cos IL)^2 = 1/L-Shell. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 Herbert.W.Kroehl@noaa.gov Geocentric and Stasiewicz Corrected DMSP-F07 Orbit Data 15 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : SSJ4 : SSJ4 : 07SE High Energy SSJ/4 Electrons New VIDF cloned from 08SE Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F07 High and Low Energy SSJ/4 Electrons 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : SSJ4 : SSJ4 : 07SE Low Energy SSJ/4 Electrons New VIDF cloned from 08SE Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F07 High and Low Energy SSJ/4 Electrons 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : SSJ4 : SSJ4 : 07SI High Energy SSJ/4 Protons New VIDF cloned from 09SI Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F07 High and Low Energy SSJ/4 Protons 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F07 : SSJ4 : SSJ4 : 07SI Low Energy SSJ/4 Protons New VIDF cloned from 09SI Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F07 High and Low Energy SSJ/4 Protons 60 1983-12-01 12:08:08 1988-04-26 12:19:00 DMSP : DMSP-F08 : OA : OA : 08OA Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Corrected Geographic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Corrected Geographic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Hakura/Gustaffson Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OA Hakura/Gustaffson Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F08 Orbit Data 15 1991-07-03 03:00:52 1992-10-31 03:28:46 DMSP : DMSP-F08 : OA : OA : 08OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : OA : OA : 08OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F08 Orbit Data 15 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : SSJ4 : SSJ4 : 08SE High Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F08 High and Low Energy SSJ/4 Electrons 60 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : SSJ4 : SSJ4 : 08SE Low Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F08 High and Low Energy SSJ/4 Electrons 60 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : SSJ4 : SSJ4 : 08SI High Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F08 High and Low Energy SSJ/4 Protons 60 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F08 : SSJ4 : SSJ4 : 08SI Low Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F08 High and Low Energy SSJ/4 Protons 60 1987-06-25 06:10:00 1994-08-01 10:30:33 DMSP : DMSP-F09 : OA : OA : 09OA Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Corrected Geographic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Corrected Geographic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Hakura/Gustaffson Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OA Hakura/Gustaffson Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F09 Orbit Data 15 1990-12-14 09:41:15 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : OA : OA : 09OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F09 Orbit Data 15 1988-02-08 03:50:00 1992-04-03 10:15:29 DMSP : DMSP-F09 : SSJ4 : SSJ4 : 09SE High Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F09 High and Low Energy SSJ/4 Electrons 60 1988-02-08 03:50:00 1992-04-03 10:15:27 DMSP : DMSP-F09 : SSJ4 : SSJ4 : 09SE Low Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F09 High and Low Energy SSJ/4 Electrons 60 1988-02-08 03:50:00 1992-04-03 10:15:27 DMSP : DMSP-F09 : SSJ4 : SSJ4 : 09SI High Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F09 High and Low Energy SSJ/4 Protons 60 1988-02-08 03:50:00 1992-04-03 10:15:27 DMSP : DMSP-F09 : SSJ4 : SSJ4 : 09SI Low Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F09 High and Low Energy SSJ/4 Protons 60 1988-02-08 03:50:00 1992-04-03 10:15:27 DMSP : DMSP-F10 : OA : OA : 10OA Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Corrected Geographic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Corrected Geographic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Hakura/Gustaffson Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OA Hakura/Gustaffson Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1992-10-31 05:24:16 DMSP : DMSP-F10 : OA : OA : 10OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F10 Orbit Data 60 1990-12-19 08:27:22 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : OA : OA : 10OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F10 Orbit Data 15 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : SSJ4 : SSJ4 : 10SE High Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 TABLE 12: threshold count level Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F10 High and Low Energy SSJ/4 Electrons 60 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : SSJ4 : SSJ4 : 10SE Low Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 TABLE 12: threshold count level Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F10 High and Low Energy SSJ/4 Electrons 60 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : SSJ4 : SSJ4 : 10SI High Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F10 High and Low Energy SSJ/4 Protons 60 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F10 : SSJ4 : SSJ4 : 10SI Low Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F10 High and Low Energy SSJ/4 Protons 60 1990-12-18 01:57:07 1997-11-14 06:36:54 DMSP : DMSP-F11 : OA : OA : 11OA Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Corrected Geographic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Corrected Geographic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Hakura/Gustaffson Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OA Hakura/Gustaffson Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and Hakura/Gustaffson values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 Corrected Geographic Latitude 10*degrees 4 Corrected Geographic Longitude 10*degrees 5 Hakura/Gustaffson Corrected Geomagnetic Latitude 10*degrees 6 Hakura/Gustaffson Corrected Geomagnetic Longitude 10*degrees One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and Hakura/Gustaffson Model Corrected DMSP-F11 Orbit Data 15 1991-12-23 02:23:55 1992-10-31 04:55:15 DMSP : DMSP-F11 : OA : OA : 11OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F11 Orbit Data 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : OA : OA : 11OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F11 Orbit Data 15 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : SSJ4 : SSJ4 : 11SE High Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F11 High and Low Energy SSJ/4 Electrons 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : SSJ4 : SSJ4 : 11SE Low Energy SSJ/4 Electrons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F11 High and Low Energy SSJ/4 Electrons 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : SSJ4 : SSJ4 : 11SI High Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F11 High and Low Energy SSJ/4 Protons 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F11 : SSJ4 : SSJ4 : 11SI Low Energy SSJ/4 Protons The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F11 High and Low Energy SSJ/4 Protons 60 1991-12-13 06:20:07 2000-05-16 05:23:34 DMSP : DMSP-F12 : OA : OA : 12OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F12 Orbit Data 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : OA : OA : 12OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F12 Orbit Data 15 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : SSJ4 : SSJ4 : 12SE High Energy SSJ/4 Electrons Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F12 High and Low Energy SSJ/4 Electrons 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : SSJ4 : SSJ4 : 12SE Low Energy SSJ/4 Electrons Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F12 High and Low Energy SSJ/4 Electrons 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : SSJ4 : SSJ4 : 12SI High Energy SSJ/4 Protons Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F12 High and Low Energy SSJ/4 Protons 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F12 : SSJ4 : SSJ4 : 12SI Low Energy SSJ/4 Protons Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F12 High and Low Energy SSJ/4 Protons 60 1994-10-01 12:14:08 2001-12-12 11:40:01 DMSP : DMSP-F13 : OA : OA : 13OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F13 Orbit Data 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : OA : OA : 13OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F13 Orbit Data 15 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : SSJ4 : SSJ4 : 13SE High Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F13 High and Low Energy SSJ/4 Electrons 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : SSJ4 : SSJ4 : 13SE Low Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F13 High and Low Energy SSJ/4 Electrons 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : SSJ4 : SSJ4 : 13SI High Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F13 High and Low Energy SSJ/4 Protons 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F13 : SSJ4 : SSJ4 : 13SI Low Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F13 High and Low Energy SSJ/4 Protons 60 1995-04-23 10:42:43 2005-02-08 11:39:07 DMSP : DMSP-F14 : OA : OA : 14OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F14 Orbit Data 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : OA : OA : 14OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F14 Orbit Data 15 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : SSJ4 : SSJ4 : 14SE High Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith Table 0 fixed 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F14 High and Low Energy SSJ/4 Electrons 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : SSJ4 : SSJ4 : 14SE Low Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith Table 0 fixed 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F14 High and Low Energy SSJ/4 Electrons 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : SSJ4 : SSJ4 : 14SI High Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith Table 0 fixed 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F14 High and Low Energy SSJ/4 Protons 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F14 : SSJ4 : SSJ4 : 14SI Low Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith Table 0 fixed 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F14 High and Low Energy SSJ/4 Protons 60 1997-04-28 02:58:28 2005-02-08 11:34:14 DMSP : DMSP-F15 : OA : OA : 15OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F15 Orbit Data 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : OA : OA : 15OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F15 Orbit Data 15 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : SSJ4 : SSJ4 : 15SE High Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F15 High and Low Energy SSJ/4 Electrons 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : SSJ4 : SSJ4 : 15SE Low Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F15 High and Low Energy SSJ/4 Electrons 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : SSJ4 : SSJ4 : 15SI High Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F15 High and Low Energy SSJ/4 Protons 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F15 : SSJ4 : SSJ4 : 15SI Low Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith Tables 0, 2 and 3 updated 11/1/04 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F15 High and Low Energy SSJ/4 Protons 60 1999-12-17 05:48:29 2005-02-08 11:41:58 DMSP : DMSP-F16 : OA : OA : 16OB Geodetic Latitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OB Geodetic Longitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OB Altitude The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OB PACE Model Corr/Geomag/Lat The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OB PACE Model Cor/Geomag/Long The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OB PACE Model MLT The conversion from integer to floating point is accomplished by the application of the look-up table. Numbers are stored in integer form which is 10 times the floating point number (or the true number). Thus, the precision of and O/A quantity is at best 0.1 of the true quantity. Geographic and PACE Model values have precision determined by NOAA to be 0.1 Degree and the Altitude precision is 1 km from NOAA. They are included in the DMSP O/A data and are included in this data set. The VIDF sensors defined are as follows: Sensor Sensor Name IDF units Number 0 Geodetic Latitude 10*degrees 1 Geodetic Longitude 10*degrees 2 Altitude nautical miles 3 PACE Model Corrected Geomagnetic Latitude 10*degrees 4 PACE Model Corrected Geomagnetic Longitude 10*degrees 5 PACE Model Magnetic Local Time (MLT) One table is included to translate all sensor units. Angular measure is converted to degrees and distance is converted to km. The following table is included in this VIDF: TABLE 0: converts to degrees and km Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geodetic and PACE Model Corrected DMSP-F16 Orbit Data 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : OA : OA : 16OC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP Geocentric and Stasiewicz Corrected DMSP-F16 Orbit Data 15 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : SSJ4 : SSJ4 : 16SE High Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F16 High and Low Energy SSJ/4 Electrons 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : SSJ4 : SSJ4 : 16SE Low Energy SSJ/4 Electrons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F16 High and Low Energy SSJ/4 Electrons 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : SSJ4 : SSJ4 : 16SI High Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F16 High and Low Energy SSJ/4 Protons 60 2003-10-24 02:47:53 2005-02-08 11:32:50 DMSP : DMSP-F16 : SSJ4 : SSJ4 : 16SI Low Energy SSJ/4 Protons Tables updated 9/26/00 by Wayne Keith The conversion to various units is accomplished by the application of different sets of look up tables. The data stored in this IDF is in compressed format (9-bit) and the tables are designed to work with the data in this form. The following is a list of tables included in this VIDF: TABLE 0: a table of center energies (eV) TABLE 1: telemetry count lookup table (compressed to uncompressed) TABLE 2: energy dependent geometric factor (cm**2-ster-keV) TABLE 3: differential number flux (cnts/cm**2-ster-s-keV) TABLE 4: number flux (cnts/cm**2-s) TABLE 5: energy flux (keV/cm**2-s) TABLE 6: energy density (keV/cm**3) TABLE 7: distribution function (s**3/cm**6) TABLE 8: number of centimeters**6 in a meter**6 TABLE 9: number of meters**6 in a kilometer**6 TABLE 10: number of eV in a keV TABLE 11: number of eV in an erg The following units can be derived from the tables. The format is to give the tables applied followed by the operations and unit definitions. DTYPE TABLES OPERS UNITS SCAN 0 0 eV SCAN 0,10 0,4 keV SCAN 0,11 0,4 erg SWEEP 1 0 counts/acc SWEEP 1 150 counts/sec SWEEP 1,3 0,3 cnts/(cm**2-s-ster-keV) SWEEP 1,3,10 0,3,4 cnts/(cm**2-s-ster-eV) SWEEP 1,3,10,0 0,3,4,3 eV/(cm**2-s-ster-eV) SWEEP 1,3,0,10 0,3,3,4 keV/(cm**2-s-ster-keV) SWEEP 1,3,0,11 0,3,3,3 ergs/(cm**2-s-ster-keV) SWEEP 1,3,0,11,10 0,3,3,3,4 ergs/(cm**2-s-ster-eV) SWEEP 1,4 0,3 counts/(cm**2-s) SWEEP 1,5 0,3 keV/(cm**2-s) SWEEP 1,5,10 0,3,3 eV/(cm**2-s) SWEEP 1,5,10,11 0,3,3,3 ergs/(cm**2-s) SWEEP 1,6 0,3 keV/(cm**3) SWEEP 1,6,10 0,3,3 eV/(cm**3) SWEEP 1,6,10,11 0,3,3,3 ergs/(cm**3) SWEEP 1,7 0,3 sec**3/cm**6 SWEEP 1,7,8 0,3,3 sec**3/m**6 SWEEP 1,7,8,9 0,3,3,3 sec**3/km**6 The quality parameter is set to the greatest value appearing within the energy sweep. Dr. Herb Kroehl NOAA E16C2 325 Broadway Bolder, CO 80303 (303) 497-6121 SPAN: KRYOS::KROEHL.M:75:SP DMSP-F16 High and Low Energy SSJ/4 Protons 60 2003-10-24 02:47:53 2005-02-08 11:32:50 FREJA : FREJA : F3H : TICS : TICS Sector 1 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Sector 2 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Sector 3 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Sector 4 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Sector 5 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Sector 6 Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Parallel Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Anti-parallel Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 FREJA : FREJA : F3H : TICS : TICS Perpendicular Olle Norberg IRF IRF IRF IRF 1 1994-01-01 12:00:00 1994-01-01 12:00:00 GeoSolarInd : INDICES : 3-HOUR : 3-HOUR : GMKA 3-Hr Kp GeoSolarInd:INDICES:3-HOUR:3-HOUR:GMKA From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS THREE-HOUR-RANGE INDEX: K indices isolate solar particle effects on the earth's magnetic field; over a 3-hour period they classify into disturbance levels the range of variation of the more unsettled horizontal field component. Each activity level relates almost logarithmically to its corresponding disturbance level. Three-hour indices discriminate conservatively between true magnetic field perturbations and quiet-day variations produced by ionospheric currents. K indices range in 28 steps from 0 (quiet) to 9 (greatly disturbed) with fractional parts expressed in 1/3 of a unit. A K-value equal to 2.666, for example, means 3-; a K-value equal to 3 means 3 exactly; and a K-value equal to 3.333 means 3+. EQUIVALENT AMPLITUDE: The a-index ranges from 0 to 400 and represents a K-value converted to a linear scale in gammas (nT), a scale that measures equivalent disturbance amplitude of a station at which K=9 has a lower limit of 400 gammas. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensor 0 to floating point. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 0 0 3Hr Kp integer Sweep 1 - - 3Hr Ap integer C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 3 Hour Kp and Ap Indicies 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : 3-HOUR : 3-HOUR : GMKA 3-Hr Ap GeoSolarInd:INDICES:3-HOUR:3-HOUR:GMKA From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS THREE-HOUR-RANGE INDEX: K indices isolate solar particle effects on the earth's magnetic field; over a 3-hour period they classify into disturbance levels the range of variation of the more unsettled horizontal field component. Each activity level relates almost logarithmically to its corresponding disturbance level. Three-hour indices discriminate conservatively between true magnetic field perturbations and quiet-day variations produced by ionospheric currents. K indices range in 28 steps from 0 (quiet) to 9 (greatly disturbed) with fractional parts expressed in 1/3 of a unit. A K-value equal to 2.666, for example, means 3-; a K-value equal to 3 means 3 exactly; and a K-value equal to 3.333 means 3+. EQUIVALENT AMPLITUDE: The a-index ranges from 0 to 400 and represents a K-value converted to a linear scale in gammas (nT), a scale that measures equivalent disturbance amplitude of a station at which K=9 has a lower limit of 400 gammas. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensor 0 to floating point. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 0 0 3Hr Kp integer Sweep 1 - - 3Hr Ap integer C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 3 Hour Kp and Ap Indicies 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : 3-HOUR : 3-HOUR : PCT3 3-Hr Avg Thule PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the northern hemisphere (the station Vostok at 83.3 degrees geomagnetic invariant latitude does the same in the southern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Thule averaged every 15 minutes over the period of 3 hour. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The 3-hour PC value is an average of the 15 minute PC indicies. This data is for the Thule station only. In February 2000 a minor typo was discovered in the old FORTRAN code used routinely for interpolation of normalization coefficients through a UT day. This typo forced only a single value of each parameter (that is, the optimal direction angle, slope, and intercept) to be taken for calculations of the index through the entire UT day. That caused introduction of an artificial daily variation in the calculated PCN index values for 1975 - 1999 and for the first two months of year 2000. This error was discovered in studying an effective area of the PCN index undertaken jointly by V. O. Papitashvili, O. Rasmussen, L. I. Gromova, V. A. Popov, and S. Vennerstrom. This inadvertently introduced error has been corrected and the entire, 25-year long time series of PCN index recalculated. The old and revised indices were compared. This comparison revealed that the correlation between the OLD and NEW time series reaches 0.99 and the correspondence between these series is satisfactory. Therefore, it was concluded that the contribution to the PCN index from the artificially introduced daily variation was negligible and all studies made in the past with the slightly contaminated PCN index are valid because the index's physical meaning has not been flawed. This is the corrected PCN (PC-Thule) data. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 3 Hour Thule Polar Cap (PC) Index 1 1975-01-01 12:00:00 2002-11-19 12:00:00 GeoSolarInd : INDICES : 3-HOUR : 3-HOUR : PCV3 3-Hr Avg Vostok PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Vostok at 83.3 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the southern hemisphere (the station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, does the same in the northern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Vostok averaged every 15 minutes over a three hour period. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The 3-hour PC value is an average of the 15 minute PC indicies. This data is for the Vostok station only. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 3 Hour Vostok Polar Cap (PC) Index 1 1978-01-01 12:00:00 1999-03-29 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : DSTD Avg Dst Dst INDICES -> Dst (Disturbance Storm Time) equivalent equatorial magnetic disturbance indices are derived from hourly scalings of low-latitude horizontal magnetic variation. They show the effect of the globally symmetrical westward flowing high altitude equatorial ring current, which causes the "main phase" depression worldwide in the H-component field during large magnetic storms. The hourly indices for the period 1 Jan 1957 through 30 Sep 1992, as derived by M. Sugiura and T. Kamei, WDC-C2 for Geomagnetism, Faculty of Science, Kyoto University, Kyoto 606, Japan. Hourly H-component magnetic variations are analyzed to remove annual secular change trends from records of a worldwide array of low-latitude observatories. A cosine factor of the site latitude transforms residual variations to their equatorial equivalents and harmonic analysis isolates the term used as the Dst index. Sugiura described Dst derivation in ANNALS OF THE IGY. The daily Dst value is an average of the hourly Dst indicies. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Day Dst (Disturbance Storm Time) Index 1 1957-01-01 12:00:00 2006-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI Bar Solar Rot# GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI Bar Solar Rot Day GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI Sum Kp GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI <Ap> GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI Cp GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI C9 GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI SunSpots GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI F10.7 GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : GMDI F10.7 Qual GeoSolarInd:INDICES:DAILY:DAILY:GMDI From data distributed by National Geophysical Data Center NATIONAL GEOPHYSICAL DATA CENTER 325 Broadway Mail Code E/GC2 Boulder, Colorado 80303-3328 USA Telephone: (303) 497-6346 FAX: (303) 497-6513 WORLDWIDE INDICES The subscript p means planetary and designates a global magnetic activity index. The following 13 observatories, which lie between 46 and 63 deg N and S geomagnetic latitude, now contribute to the planetary indices: Lerwick (UK), Eskdalemuir (UK), Hartland (UK), Ottawa (Canada), Fredericksburg (USA), Meannook (Canada), Sitka (USA), Eyrewell (NZ), Canberra (Australia), Lovo (Sweden), Rude Skov (Denmark), Wingst (Germany), and Witteveen (Netherlands). SELECTED SENSOR DESCRIPTIONS BARTELS SOLAR ROTATION NUMBER: a sequence of 27-day intervals counted continuously from February 8, 1832. Cp or PLANETARY DAILY CHARACTER FIGURE: a qualitative estimate of overall level of magnetic activity for the day determined from the sum of the eight ap amplitudes. Cp ranges, in steps of one-tenth, from 0 (quiet) to 2.5 (highly disturbed). C9: a conversion of the 0-to-2.5 range of the Cp index to one digit between 0 and 9. INTERNATIONAL SUNSPOT NUMBER: the Zurich sunspot number thru Dec. 31, 1980, and the International Brussels number thereafter. OTTAWA 10.7-CM SOLAR RADIO FLUX ADJUSTED TO 1 AU: measured at 1700 UT daily and expressed in units of 10**-22 Watts/m**2/Hz. Observations began on 2/14/47. From that date thru 12/31/73 the fluxes given here don't reflect revisions Ottawa made in 1966. FLUX QUALIFIER: "0" indicates flux required no adjustment; "1" indicates flux required adjustment for burst in progress at time of measurement; "2" indicates a flux approximated by either interpolation or extrapolation; and "3" indicates no observation. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry of sensors 2 and 4 to floating point and from sensor 7 to watts/m**2/Hz TABLE 1: polynomial coefficient converting summed Kp in sensor 2 to average Kp between 0 and 9 and polynomial coeff. for converting sensor 7 to sfu units. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS DESC UNIT Sweep 0 - - Rotation Number integer Sweep 1 - - Rotation Day day Sweep 2 0 0 Sum Kp integer Sweep 2 0,1 0,3 Avg Kp integer Sweep 3 - - Avg Ap gamma Sweep 4 0 0 Cp integer Sweep 5 - - C9 integer Sweep 6 - - Sun Spots integer Sweep 7 0 0 10.7 cm flux watts/m**2/Hz Sweep 8 - - 10.7 cm qual integer Sweep 7 1 0 10.7 cm flux sfu C. Gurgiolo Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 chris@bilbo.space.swri.edu 1 Day F10.7, C9, Sunspot Number, CP, Solar Rotation Numbers 10 1932-01-01 12:00:00 2005-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : MGIID MgII The NOAA Mg II daily Index version 9.1 -> This vertual containes the Mg Core to wing ratio scaled to the NOAA9/Nimbus7 data with blanks for missing data. The Mg II core-to-wing ratio is derived by taking the ratio of the h and k lines of the solar Mg II feature at 280 nm to the background or wings at approximately 278 nm and 282 nm. The h and k lines are variable chromospheric emissions while the background emissions are more stable. The result is a robust measure of chromospheric activity. This ratio has been shown to be a good measure of solar UV and EUV emissions. Each of the data sets was scaled to the original NOAA TIROS NOAA 9 data set with a linear fit of the overlapping data. The nature of the Mg II core-to-wing ratio and the quality of the data resulted in linear correlation coefficients between 0.98 and 0.999. The source of the data is: 1 - NOAA TIROS and NOAA 9 Data (previously released) 2 = NOAA 11 Data 3 - NOAA 9 (Alternate Algorithm) 4 = UARS Solstice Data 5 - GOME Data 6 - NOAA 16 Acknowledgements: Tom Woods (CU LASP), Gary Rottman (CU LASP), and Giuliana de Toma (NCAR, HAO) for the SOLSTICE data. Mark Weber (U. Bremen, Germany) for the GOME data. References: Viereck and Puga, The NOAA Mg II core-to-wing solar index: Construction of a 20-year time series of chromospheric variability from multiple satellites., JGR, 104, pp9995-10005, May 1999. Viereck et al., The Mg II Index: A proxy for Solar EUV., GRL, 28, pp1343-1346, April 2001. Lawrence Puga and Rodney Viereck U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Lawrence.Puga@noaa.gov or Rodney.Viereck@noaa.gov 1 Day Mg II Core-to-Wing Ratio 1 1978-11-07 12:00:00 1978-11-07 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : MGIID MgII Data The NOAA Mg II daily Index version 9.1 -> This vertual containes the Mg Core to wing ratio scaled to the NOAA9/Nimbus7 data with blanks for missing data. The Mg II core-to-wing ratio is derived by taking the ratio of the h and k lines of the solar Mg II feature at 280 nm to the background or wings at approximately 278 nm and 282 nm. The h and k lines are variable chromospheric emissions while the background emissions are more stable. The result is a robust measure of chromospheric activity. This ratio has been shown to be a good measure of solar UV and EUV emissions. Each of the data sets was scaled to the original NOAA TIROS NOAA 9 data set with a linear fit of the overlapping data. The nature of the Mg II core-to-wing ratio and the quality of the data resulted in linear correlation coefficients between 0.98 and 0.999. The source of the data is: 1 - NOAA TIROS and NOAA 9 Data (previously released) 2 = NOAA 11 Data 3 - NOAA 9 (Alternate Algorithm) 4 = UARS Solstice Data 5 - GOME Data 6 - NOAA 16 Acknowledgements: Tom Woods (CU LASP), Gary Rottman (CU LASP), and Giuliana de Toma (NCAR, HAO) for the SOLSTICE data. Mark Weber (U. Bremen, Germany) for the GOME data. References: Viereck and Puga, The NOAA Mg II core-to-wing solar index: Construction of a 20-year time series of chromospheric variability from multiple satellites., JGR, 104, pp9995-10005, May 1999. Viereck et al., The Mg II Index: A proxy for Solar EUV., GRL, 28, pp1343-1346, April 2001. Lawrence Puga and Rodney Viereck U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Lawrence.Puga@noaa.gov or Rodney.Viereck@noaa.gov 1 Day Mg II Core-to-Wing Ratio 1 1978-11-07 12:00:00 1978-11-07 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : PCTD Avg Thule PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the northern hemisphere (the station Vostok at 83.3 degrees geomagnetic invariant latitude does the same in the southern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Thule averaged every 15 minutes over the entire day. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The daily PC value is an average of the 15 minute PC indicies. This data is for the Thule station only. In February 2000 a minor typo was discovered in the old FORTRAN code used routinely for interpolation of normalization coefficients through a UT day. This typo forced only a single value of each parameter (that is, the optimal direction angle, slope, and intercept) to be taken for calculations of the index through the entire UT day. That caused introduction of an artificial daily variation in the calculated PCN index values for 1975 - 1999 and for the first two months of year 2000. This error was discovered in studying an effective area of the PCN index undertaken jointly by V. O. Papitashvili, O. Rasmussen, L. I. Gromova, V. A. Popov, and S. Vennerstrom. This inadvertently introduced error has been corrected and the entire, 25-year long time series of PCN index recalculated. The old and revised indices were compared. This comparison revealed that the correlation between the OLD and NEW time series reaches 0.99 and the correspondence between these series is satisfactory. Therefore, it was concluded that the contribution to the PCN index from the artificially introduced daily variation was negligible and all studies made in the past with the slightly contaminated PCN index are valid because the index's physical meaning has not been flawed. This is the corrected PCN (PC-Thule) data. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Day Thule Polar Cap (PC) Index 1 1975-01-01 12:00:00 2002-11-19 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : PCVD Avg Vostok PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Vostok at 83.3 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the southern hemisphere (the station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, does the same in the northern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Vostok averaged every 15 minutes over the entire day. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The daily PC value is an average of the 15 minute PC indicies. This data is for the Vostok station only. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Day Vostok Polar Cap (PC) Index 1 1978-01-01 12:00:00 1999-03-29 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 Julian Day The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 F10.7 The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 81-Day Avg. F10.7 The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 Lyman-a The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 81-Day Avg. Lyman-a The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 E10.7 The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 81-Day Avg. E10.7 The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : DAILY : DAILY : SO2000 SOLAR2000 Solar Flux The SOLAR2000 Daily Nowcast Solar Irradiances and E10.7 are a joint product of Space Environment Technologies (SET/SpaceWx) and the NOAA Space Environment Center. These operational data are produced through a Cooperative Research and Development Agreement (CRADA) signed on May 2, 2000 by both parties. Liabilities and authorized uses are described in the CRADA. The NOAA/SEC CRADA point of contact for the Space Environment SOLAR2000 is Dr. Rodney Viereck (Rodney.Viereck@noaa.gov). At dditional information about SpaceWx and the SOLAR2000 model, including an anonymous ftp location to retrieve SOLAR2000 data files, and a downloadable IDL GUI application for the Research Grade model, can be found at http://SpaceWx.com. SpaceWx points of contact are: Dr. W. Kent Tobiska, CEO/Chief Scientist (ktobiska@spacenvironment.net) S. Dave Bouwer, Chief Engineer (David.Bouwer@noaa.gov). Rodney Viereck, Dr. W. Kent Tobiska, or S. Dave Bouwer U.S. Dept. of Commerce NOAA, Space Environment Center Boulder, CO 80303-3328 Rodney.Viereck@noaa.gov, ktobiska@spacenvironment.net, David.Bouwer@noaa.gov 1 1947-02-14 12:00:00 2000-01-01 12:00:00 GeoSolarInd : INDICES : HOURLY : HOURLY : DSTH Dst Dst INDICES -> Dst (Disturbance Storm Time) equivalent equatorial magnetic disturbance indices are derived from hourly scalings of low-latitude horizontal magnetic variation. They show the effect of the globally symmetrical westward flowing high altitude equatorial ring current, which causes the "main phase" depression worldwide in the H-component field during large magnetic storms. The hourly indices for the period 1 Jan 1957 through 30 Sep 1992, as derived by M. Sugiura and T. Kamei, WDC-C2 for Geomagnetism, Faculty of Science, Kyoto University, Kyoto 606, Japan. Hourly H-component magnetic variations are analyzed to remove annual secular change trends from records of a worldwide array of low-latitude observatories. A cosine factor of the site latitude transforms residual variations to their equatorial equivalents and harmonic analysis isolates the term used as the Dst index. Sugiura described Dst derivation in ANNALS OF THE IGY. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Hour Dst (Disturbance Storm Time) Index 1 1957-01-01 12:00:00 2006-01-01 12:00:00 GeoSolarInd : INDICES : HOURLY : HOURLY : PCTH Hr Avg Thule PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the northern hemisphere (the station Vostok at 83.3 degrees geomagnetic invariant latitude does the same in the southern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Thule averaged every 15 minutes over the period of 1 hour. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The hourly PC value is an average of the 15 minute PC indicies. This data is for the Thule station only. In February 2000 a minor typo was discovered in the old FORTRAN code used routinely for interpolation of normalization coefficients through a UT day. This typo forced only a single value of each parameter (that is, the optimal direction angle, slope, and intercept) to be taken for calculations of the index through the entire UT day. That caused introduction of an artificial daily variation in the calculated PCN index values for 1975 - 1999 and for the first two months of year 2000. This error was discovered in studying an effective area of the PCN index undertaken jointly by V. O. Papitashvili, O. Rasmussen, L. I. Gromova, V. A. Popov, and S. Vennerstrom. This inadvertently introduced error has been corrected and the entire, 25-year long time series of PCN index recalculated. The old and revised indices were compared. This comparison revealed that the correlation between the OLD and NEW time series reaches 0.99 and the correspondence between these series is satisfactory. Therefore, it was concluded that the contribution to the PCN index from the artificially introduced daily variation was negligible and all studies made in the past with the slightly contaminated PCN index are valid because the index's physical meaning has not been flawed. This is the corrected PCN (PC-Thule) data. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Hour Thule Polar Cap (PC) Index 1 1975-01-01 12:00:00 2002-11-19 12:00:00 GeoSolarInd : INDICES : HOURLY : HOURLY : PCVH Hr Avg Vostok PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Vostok at 83.3 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the southern hemisphere (the station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, does the same in the northern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Vostok averaged every 15 minutes over each hour. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. The hourly PC value is an average of the 15 minute PC indicies. This data is for the Vostok station only. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Hour Vostok Polar Cap (PC) Index 1 1978-01-01 12:00:00 1999-03-29 12:00:00 GeoSolarInd : INDICES : MINUTE : MINUTE : PCT1 1-Min Thule PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the northern hemisphere (the station Vostok at 83.3 degrees geomagnetic invariant latitude does the same in the southern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Thule every 1 minute. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. This PC index value is the 1 minute PC for the Thule station only. In February 2000 a minor typo was discovered in the old FORTRAN code used routinely for interpolation of normalization coefficients through a UT day. This typo forced only a single value of each parameter (that is, the optimal direction angle, slope, and intercept) to be taken for calculations of the index through the entire UT day. That caused introduction of an artificial daily variation in the calculated PCN index values for 1975 - 1999 and for the first two months of year 2000. This error was discovered in studying an effective area of the PCN index undertaken jointly by V. O. Papitashvili, O. Rasmussen, L. I. Gromova, V. A. Popov, and S. Vennerstrom. This inadvertently introduced error has been corrected and the entire, 25-year long time series of PCN index recalculated. The old and revised indices were compared. This comparison revealed that the correlation between the OLD and NEW time series reaches 0.99 and the correspondence between these series is satisfactory. Therefore, it was concluded that the contribution to the PCN index from the artificially introduced daily variation was negligible and all studies made in the past with the slightly contaminated PCN index are valid because the index's physical meaning has not been flawed. This is the corrected PCN (PC-Thule) data. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Minute Thule Polar Cap (PC) Index 1 1975-01-01 12:00:00 2002-11-19 12:00:00 GeoSolarInd : INDICES : MINUTE : MINUTE : PCTM Thule PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the northern hemisphere (the station Vostok at 83.3 degrees geomagnetic invariant latitude does the same in the southern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Thule every 15 minutes. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. This PC index value is the 15 minute PC for the Thule station only. In February 2000 a minor typo was discovered in the old FORTRAN code used routinely for interpolation of normalization coefficients through a UT day. This typo forced only a single value of each parameter (that is, the optimal direction angle, slope, and intercept) to be taken for calculations of the index through the entire UT day. That caused introduction of an artificial daily variation in the calculated PCN index values for 1975 - 1999 and for the first two months of year 2000. This error was discovered in studying an effective area of the PCN index undertaken jointly by V. O. Papitashvili, O. Rasmussen, L. I. Gromova, V. A. Popov, and S. Vennerstrom. This inadvertently introduced error has been corrected and the entire, 25-year long time series of PCN index recalculated. The old and revised indices were compared. This comparison revealed that the correlation between the OLD and NEW time series reaches 0.99 and the correspondence between these series is satisfactory. Therefore, it was concluded that the contribution to the PCN index from the artificially introduced daily variation was negligible and all studies made in the past with the slightly contaminated PCN index are valid because the index's physical meaning has not been flawed. This is the corrected PCN (PC-Thule) data. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 15 Minute Vostok Polar Cap (PC) Index 1 1975-01-01 12:00:00 2002-11-19 12:00:00 GeoSolarInd : INDICES : MINUTE : MINUTE : PCV1 1-Min Vostok PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Vostok at 83.3 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the southern hemisphere (the station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, does the same in the northern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Vostok every 1 minute. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. This 1 minute PC index is from the Vostok station only. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 1 Minute Vostok Polar Cap (PC) Index 1 1992-01-01 12:00:00 1999-03-29 12:00:00 GeoSolarInd : INDICES : MINUTE : MINUTE : PCVM Vostok PC GEOMAGNETIC POLAR CAP INDEX -> Geomagnetic Polar Cap (PC) Index -- PC is an index for magnetic activity in the (P)olar (C)ap. It is based on data from a single nearpole station, and aimed to monitor the polar cap magnetic activity generated by such solar wind parameters as the southward component of the interplanetary magnetic field (IMF), the azimuthal component of the IMF (By), and the solar wind velocity v. The station Vostok at 83.3 degrees geomagnetic invariant latitude, fulfills the requirement of being close to the magnetic pole in the southern hemisphere (the station Thule, located in the village Qaanaaq in Greenland at 86.5 degrees geomagnetic invariant latitude, does the same in the northern hemisphere). The PC index is derived independently for the two stations. This file contains the PC index for Vostok every 15 minutes. The PC-index is based on an idea by Troshichev et al. (1979) and developed in papers by Troshichev and Andrezen (1985), Vennerstrom and Friis-Christensen (1989), Troshichev et al. (1988), Vennerstrom (1991), and Vennerstrom et al. (1991). Earlier data for 1975-1982 appear in Troshichev et al. (1991). The data from 1975 to 1993 are published in Report UAG-103. Monthly plots from Thule appear regularly in SGD since October 1993. This 15 minute PC index is from the Vostok station only. Les Morris National Geophysical Data Center Solar Terrestrial Physics Division Boulder, CO 80303-3328 (303) 497-6475 [Internet: lmorris@ngdc.noaa.gov] 15 Minute Thule Polar Cap (PC) Index 1 1978-01-01 12:00:00 1999-03-29 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 HP /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 HE /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 HN /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 HT /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 Theta /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD1 GOES-06 Phi /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 1 minute and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 HP /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 HE /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 HN /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 HT /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 Theta /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : MAGNETIC_FIELD : G06BFLD5 GOES-06 Phi /* This virtual contains the GOES magnetic field for GOES-06. The magnetic /* field is averaged every 5 minutes and reported. The GOES-06 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASCL5 GOES-06 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-06. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ASPC5 GOES-06 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 alpha particle spectra at 5 minute resolution 6 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ELEC1 GOES-06 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-06. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral electron channel at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06ELEC5 GOES-06 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-06. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral electron channel at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PINT5 GOES-06 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-06. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSH5 GOES-06 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected high-range proton differential spectra at 5 minute resolution 3 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSL1 GOES-06 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSL1 GOES-06 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSL5 GOES-06 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSL5 GOES-06 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-06. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PSPC5 GOES-06 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-06. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 integral proton spectra at 5 minute resolution 6 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC1 GOES-06 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : PARTICLES : G06PUC5 GOES-06 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-06. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1994-11-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY1 GOES-06 XS /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1994-07-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY1 GOES-06 XL /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1994-07-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY1 GOES-06 X-ray /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1994-07-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY5 GOES-06 XS /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1994-08-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY5 GOES-06 XL /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1994-08-01 12:00:00 GOES : GOES-06 : SEM : XRAYS : G06XRAY5 GOES-06 X-ray /* This virtual contains the GOES X-ray flux for GOES-06. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-06 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-06 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1994-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 HP /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 HE /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 HN /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 HT /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 Theta /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD1 GOES-07 Phi /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 1 minute and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 HP /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 HE /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 HN /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 HT /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 Theta /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : MAGNETIC_FIELD : G07BFLD5 GOES-07 Phi /* This virtual contains the GOES magnetic field for GOES-07. The magnetic /* field is averaged every 5 minutes and reported. The GOES-07 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 magnetic field components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASCL5 GOES-07 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-07. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ASPC5 GOES-07 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-07. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 alpha particle spectra at 5 minute resolution 6 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ELEC1 GOES-07 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-07. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral electron channel at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07ELEC5 GOES-07 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-07. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral electron channel at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PINT5 GOES-07 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-07. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PSL1 GOES-07 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-07. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PSL1 GOES-07 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-07. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PSL5 GOES-07 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-07. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PSL5 GOES-07 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-07. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PSPC5 GOES-07 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-07. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 integral proton spectra at 5 minute resolution 6 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC1 GOES-07 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : PARTICLES : G07PUC5 GOES-07 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-07. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY1 GOES-07 XS /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY1 GOES-07 XL /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY1 GOES-07 X-ray /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 1 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY5 GOES-07 XS /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY5 GOES-07 XL /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-07 : SEM : XRAYS : G07XRAY5 GOES-07 X-ray /* This virtual contains the GOES X-ray flux for GOES-07. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-07 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-07 x-ray flux components at 5 minute resolution 1 1991-01-01 12:00:00 1996-08-01 12:00:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 HP /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 HE /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 HN /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 HT /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 Theta /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD1 GOES-08 Phi /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 1 minute and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 1 minute resolution 1 1995-11-29 04:24:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 HP /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 HE /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 HN /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 HT /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 Theta /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : MAGNETIC_FIELD : G08BFLD5 GOES-08 Phi /* This virtual contains the GOES magnetic field for GOES-08. The magnetic /* field is averaged every 5 minutes and reported. The GOES-08 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 magnetic field components at 5 minute resolution 1 1995-11-29 04:20:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASCL5 GOES-08 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-08. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ASPC5 GOES-08 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 alpha particle spectra at 5 minute resolution 6 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ELEC1 GOES-08 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-08. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral electron channel at 1 minute resolution 1 1995-05-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08ELEC5 GOES-08 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-08. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral electron channel at 5 minute resolution 1 1995-05-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PINT5 GOES-08 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-08. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSH5 GOES-08 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected high-range proton differential spectra at 5 minute resolution 3 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSL1 GOES-08 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSL1 GOES-08 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSL5 GOES-08 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSL5 GOES-08 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-08. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PSPC5 GOES-08 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-08. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 integral proton spectra at 5 minute resolution 6 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC1 GOES-08 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : PARTICLES : G08PUC5 GOES-08 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-08. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY1 GOES-08 XS /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY1 GOES-08 XL /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY1 GOES-08 X-ray /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 1 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY5 GOES-08 XS /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY5 GOES-08 XL /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-08 : SEM : XRAYS : G08XRAY5 GOES-08 X-ray /* This virtual contains the GOES X-ray flux for GOES-08. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-08 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-08 x-ray flux components at 5 minute resolution 1 1995-03-01 12:00:00 2003-05-05 09:15:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 HP /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 HE /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 HN /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 HT /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 Theta /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD1 GOES-09 Phi /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 1 minute and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 HP /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 HE /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 HN /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 HT /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 Theta /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : MAGNETIC_FIELD : G09BFLD5 GOES-09 Phi /* This virtual contains the GOES magnetic field for GOES-09. The magnetic /* field is averaged every 5 minutes and reported. The GOES-09 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 magnetic field components at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-01 12:00:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASCL5 GOES-09 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-09. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ASPC5 GOES-09 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 alpha particle spectra at 5 minute resolution 6 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09ELEC1 GOES-09 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-09. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral electron channel at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09ELEC5 GOES-09 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-09. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral electron channel at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PINT5 GOES-09 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-09. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PSH5 GOES-09 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected high-range proton differential spectra at 5 minute resolution 3 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PSL1 GOES-09 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PSL1 GOES-09 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PSL5 GOES-09 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PSL5 GOES-09 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-09. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PSPC5 GOES-09 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-09. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 integral proton spectra at 5 minute resolution 6 1996-04-01 12:00:00 1998-08-31 07:30:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC1 GOES-09 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:29:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : PARTICLES : G09PUC5 GOES-09 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-09. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1996-04-01 12:00:00 1998-08-31 07:25:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY1 GOES-09 XS /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 1 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY1 GOES-09 XL /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 1 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY1 GOES-09 X-ray /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 1 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY5 GOES-09 XS /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 5 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY5 GOES-09 XL /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 5 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-09 : SEM : XRAYS : G09XRAY5 GOES-09 X-ray /* This virtual contains the GOES X-ray flux for GOES-09. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-09 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-09 x-ray flux components at 5 minute resolution 1 1996-04-01 12:00:00 1998-07-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 HP /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 HE /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 HN /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 HT /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 Theta /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD1 GOES-10 Phi /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 1 minute and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 HP /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 HE /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 HN /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 HT /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 Theta /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : MAGNETIC_FIELD : G10BFLD5 GOES-10 Phi /* This virtual contains the GOES magnetic field for GOES-10. The magnetic /* field is averaged every 5 minutes and reported. The GOES-10 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 magnetic field components at 5 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASCL5 GOES-10 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-10. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle differential and integral channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ASPC5 GOES-10 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 alpha particle spectra at 5 minute resolution 6 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ELEC1 GOES-10 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-10. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral electron channel at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10ELEC5 GOES-10 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-10. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral electron channel at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PINT5 GOES-10 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-10. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton channels at 5 minute resolution 1 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSH5 GOES-10 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected high-range proton differential spectra at 5 minute resolution 3 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSL1 GOES-10 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSL1 GOES-10 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSL5 GOES-10 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSL5 GOES-10 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-10. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PSPC5 GOES-10 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-10. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 integral proton spectra at 5 minute resolution 6 1998-07-09 03:50:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC1 GOES-10 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : PARTICLES : G10PUC5 GOES-10 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-10. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 1998-07-09 03:45:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY1 GOES-10 XS /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY1 GOES-10 XL /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY1 GOES-10 X-ray /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 1 minute resolution 1 1998-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY5 GOES-10 XS /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 5 minute resolution 1 1998-07-09 02:35:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY5 GOES-10 XL /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 5 minute resolution 1 1998-07-09 02:35:00 2009-05-01 12:00:00 GOES : GOES-10 : SEM : XRAYS : G10XRAY5 GOES-10 X-ray /* This virtual contains the GOES X-ray flux for GOES-10. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-10 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-10 x-ray flux components at 5 minute resolution 1 1998-07-09 02:35:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 HP /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 HE /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 HN /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 HT /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 Theta /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD1 GOES-11 Phi /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 1 minute and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 HP /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 HE /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 HN /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 HT /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 Theta /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : MAGNETIC_FIELD : G11BFLD5 GOES-11 Phi /* This virtual contains the GOES magnetic field for GOES-11. The magnetic /* field is averaged every 5 minutes and reported. The GOES-11 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 magnetic field components at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASCL5 GOES-11 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-11. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ASPC5 GOES-11 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 alpha particle spectra at 5 minute resolution 6 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ELEC1 GOES-11 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-11. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral electron channel at 1 minute resolution 1 2001-01-01 12:03:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11ELEC5 GOES-11 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-11. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral electron channel at 5 minute resolution 1 2001-01-01 12:05:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI1 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI2 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI3 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI4 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI5 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI6 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PINT5 GOES-11 cI7 /* This virtual contains the calibrated GOES proton number flux particles /* from the integral telescope for GOES-11. The particles are averaged /* every 5 minutes and reported. The integral proton values are stored as /* floating point numbers in the units of counts/(cm**2 sec sr). This virtual /* contains the following scalar data: /* /* cI1: I1 > 1 MeV protons (Counts/cm2 sec sr) Corrected /* cI2: I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* cI3: I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* cI4: I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* cI5: I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* cI6: I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* cI7: I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSH5 GOES-11 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected high-range proton differential spectra at 5 minute resolution 3 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSL1 GOES-11 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSL1 GOES-11 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSL5 GOES-11 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSL5 GOES-11 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-11. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PSPC5 GOES-11 Derived Proton Flux /* This virtual contains the GOES proton number flux spectra in /* the form of a vector for GOES-11. The integral intensity is averaged /* every 5 minutes and reported. Differences between the proton integral /* intensity vector components are stored as floating point numbers in the units /* of counts/(cm**2 sec sr). Values between integral energies are derived from /* the difference in cutoff energies of each integral channel. This virtual /* containes the following components used to form the vector: /* /* I1 > 1 MeV protons - I2 > 5 MeV protons (Counts/cm2 sec sr) Corrected /* I2 > 5 MeV protons - I3 > 10 MeV protons (Counts/cm2 sec sr) Corrected /* I3 > 10 MeV protons - I4 > 30 MeV protons (Counts/cm2 sec sr) Corrected /* I4 > 30 MeV protons - I5 > 50 MeV protons (Counts/cm2 sec sr) Corrected /* I5 > 50 MeV protons - I6 > 60 MeV protons (Counts/cm2 sec sr) Corrected /* I6 > 60 MeV protons - I7 > 100 MeV protons (Counts/cm2 sec sr) Corrected /* /* This data is corrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 integral proton spectra at 5 minute resolution 6 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC1 GOES-11 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : PARTICLES : G11PUC5 GOES-11 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-11. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2000-07-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY1 GOES-11 XS /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 1 minute resolution 1 2001-05-30 01:19:00 2008-02-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY1 GOES-11 XL /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 1 minute resolution 1 2001-05-30 01:19:00 2008-02-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY1 GOES-11 X-ray /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 1 minute resolution 1 2001-05-30 01:19:00 2008-02-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY5 GOES-11 XS /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 5 minute resolution 1 2001-05-30 01:20:00 2008-02-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY5 GOES-11 XL /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 5 minute resolution 1 2001-05-30 01:20:00 2008-02-01 12:00:00 GOES : GOES-11 : SEM : XRAYS : G11XRAY5 GOES-11 X-ray /* This virtual contains the GOES X-ray flux for GOES-11. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-11 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-11 x-ray flux components at 5 minute resolution 1 2001-05-30 01:20:00 2008-02-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 HP /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 HE /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 HN /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 HT /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 Theta /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD1 GOES-12 Phi /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 1 minute and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 1 minute resolution 1 2003-01-07 04:37:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 HP /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 HE /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 HN /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 HT /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 Theta /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : MAGNETIC_FIELD : G12BFLD5 GOES-12 Phi /* This virtual contains the GOES magnetic field for GOES-12. The magnetic /* field is averaged every 5 minutes and reported. The GOES-12 magnetic field /* is reported as a triad of components: the magnetic flux (HP) parallel to /* the satellite spin axis, the earthward magnetic flux (HE), and the magnetic /* flux normal to HP and HE is the HN component (points West for GOES 1-4, /* East for GOES 5+). The total magnetic flux is called HT. Magnetic field /* data are stored in nanoTesla*100. Table 0 should be applied to revert /* back to nanoTesla. /* /* Angles represent the direction of the magnetic field. They are stored in /* degrees * 1000 and are also reconstructed using tabte 1. /* /* HP parallel (northward) Magnetic Flux (nanotesla) /* HE Earthward Magnetic Flux (nanotesla) /* HN Normal (eastward) Magnetic Flux (nanotesla) /* HT Total Magnetic Flux (nanotesla) /* Theta: angle from +Hn to Hp-He plane (degrees) /* Phi: angle from +Hp axis toward +He axis (degrees) NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 magnetic field components at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A1 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A2 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A3 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A4 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A5 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A6 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A7 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASCL5 GOES-12 A8 /* This virtual contains the GOES alpha-particle differential and integrated /* intensity for GOES-12. The differential and integrated intensity is /* averaged every 5 minutes and reported. The alpha-particle differential /* and integrated intensity is stored as floating point number in the units /* of counts/(cm**2 sec sr MeV). This virtual containes the following scalar /* data: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA7: A7 2560 - 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA8: A8 > 3400 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ASPC5 GOES-12 Alpha Particles /* This virtual contains the GOES alpha-particle differential intensity in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 5 minutes and reported. The alpha-particle differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uA1: A1 4.0 - 10.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA2: A2 10.0 - 21.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA3: A3 21.0 - 60.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA4: A4 60.0 - 150.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA5: A5 150.0 - 250.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* uA6: A6 300.0 - 500.0 MeV alpha-particles (Counts/cm**2 sec sr MeV) /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Alpha Channel [MeV] /* Table 1: Center Energy for each Alpha Channel [MeV] /* Table 2: High Energy Cutoff for each Alpha Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 alpha particle spectra at 5 minute resolution 6 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ELEC1 GOES-12 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-12. The electron integrated number intensity is averaged every /* 1 minute and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 integral electron channel at 1 minute resolution 1 2003-09-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12ELEC5 GOES-12 E1 /* This virtual contains the GOES electron integrated number intensity for /* GOES-12. The electron integrated number intensity is averaged every /* 5 minutes and reported. Electron integrated number intensity is stored /* as a floating point number in the units of counts/(cm**2 sec sr). This /* virtual containes the following scalar data: /* /* E1 >= 2 MeV electrons (Counts/cm2 sec sr) Corrected, but remain /* unreliable during ion storms. NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 integral electron channel at 5 minute resolution 1 2003-09-01 12:00:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PSH5 GOES-12 High-Range Protons /* This virtual contains the GOES high-range proton energy flux spectra in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 5 minutes and reported. The high-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). This virtual containes the following /* components used to form the vector: /* /* uP8: P8 350.0 - 420.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420.0 - 510.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510.0 - 700.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* /* This data is uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected high-range proton differential spectra at 5 minute resolution 3 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PSL1 GOES-12 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PSL1 GOES-12 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 1 minute and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential spectra at 1 minute resolution 7 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PSL5 GOES-12 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PSL5 GOES-12 Low-Range Protons /* This virtual contains the GOES low-range proton energy flux spectra in /* the form of a vector for GOES-12. The differential intensity is averaged /* every 5 minutes and reported. The low-range proton differential intensity /* vector components are stored as floating point numbers in the units of /* counts/(cm**2 sec sr MeV). Corrected and uncorrected proton data are stored /* as separate vectors. This virtual containes the following components used /* to form the vector: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* /* This data is both corrected and uncorrected. /* /* Table 0: Low Energy Cutoff for each Energy Channel [MeV] /* Table 1: Center Energy for each Energy Channel [MeV] /* Table 2: High Energy Cutoff for each Energy Channel [MeV] /* Table 3: Table Contains the Conversion Factor from eV to erg [erg/eV] /* Table 4: Table Contains the Constant Number 1000 for Converting Scan Values /* Table 5: This Table is Used to put the Data Value into the Math Buffer /* Table 6: Table Contains the Constant Number 1000 for Converting Data Values NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential spectra at 5 minute resolution 7 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC1 GOES-12 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 1 minute and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 1 minute resolution 1 2003-01-01 10:09:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP8 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP9 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP10 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 uP11 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP1 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP2 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP3 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP4 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP5 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP6 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : PARTICLES : G12PUC5 GOES-12 cP7 /* This virtual contains scalar values of the GOES energetic protons, both /* calibrated and uncalibrated, from both differential and integral values. /* Data is from instrumentation on GOES-12. The energetic particles are averaged /* every 5 minutes and reported. Both corrected data and uncorrected data is /* stored as floating point numbers in Intensity units of /* Counts/(cm**2 sec sr MeV). This virtual contains the following scalar data: /* /* uP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP8: P8 350 - 420 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP9: P9 420 - 510 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP10: P10 510 - 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* uP11: P11 > 700 MeV protons (Counts/cm2 sec sr MeV) Uncorrected /* cP1: P1 .8 - 4.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP2: P2 4.0 - 9.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP3: P3 9.0 - 15.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP4: P4 15.0 - 40.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP5: P5 40.0 - 80.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP6: P6 80.0 - 165.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* cP7: P7 165.0 - 500.0 MeV protons (Counts/cm2 sec sr MeV) Corrected /* NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 uncorrected and corrected low-range proton differential and integral channels at 5 minute resolution 1 2003-01-07 04:35:00 2009-05-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY1 GOES-12 XS /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 1 minute resolution 1 2003-01-10 12:48:00 2007-04-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY1 GOES-12 XL /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 1 minute resolution 1 2003-01-10 12:48:00 2007-04-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY1 GOES-12 X-ray /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 1 minute and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 1 minute resolution 1 2003-01-10 12:48:00 2007-04-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY5 GOES-12 XS /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 5 minute resolution 1 2003-01-10 12:45:00 2007-04-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY5 GOES-12 XL /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 5 minute resolution 1 2003-01-10 12:45:00 2007-04-01 12:00:00 GOES : GOES-12 : SEM : XRAYS : G12XRAY5 GOES-12 X-ray /* This virtual contains the GOES X-ray flux for GOES-12. The X-ray energy /* flux is averaged every 5 minutes and reported. GOES-12 contains two X-ray /* channels, one that covers the shorter X-ray wavelengths (labeled XS) and /* the other that covers the longer X-ray wavelengths (labeled XL). In /* addition this virtual also contains the class of the X-ray energy flux. /* The X-ray class is represented as: 0 for B, 1 for C, 2 for M and 3 for X. /* Determination of the class is based on the 1-8 Ang X-ray Flux as stated /* below. /* /* X-ray /* XS: XS .5-3 Ang X-ray Flux (Watts/Meter2) /* XL: XL 1-8 Ang X-ray Flux (Watts/Meter2) /* X-RAY FLARE CLASS: Rank of a FLARE based on its X-ray energy output. /* Flares are classified by the order of magnitude of the /* peak burst intensity (I) measured at the earth in the /* 1 to 8 angstrom band as follows: /* Class (in Watt/sq. Meter) /* B I < 1.0E-06 /* C 1.0E-06 <= I <= 1.0E-05 /* M 1.0E-05 <= I <= 1.0E-04 /* X I >= 1.0E-04 NOAA/National Weather Service National Centers for Environmental Prediction Space Environment Center, W/NP9 325 Broadway, Boulder CO 80305 http://goes.ngdc.noaa.gov/data/avg GOES-12 x-ray flux components at 5 minute resolution 1 2003-01-10 12:45:00 2007-04-01 12:00:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Magnitude (F1) Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Magnitude (F2) Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance XX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance YY Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance ZZ Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance YX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance ZX Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Variance ZY Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Inclination (Theta) Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Azimuthal (Phi) Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Theta_SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Phi_SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Bx SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG By SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Bz SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Theta_SM Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Phi_SM Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Bx SM Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG By SM Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Bz SM Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Number of Sequences Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Number of Detail Points Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Orbit Number Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Bit Rate Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMAG Pseudo Sequence Count Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 IMF Magnetic Field as Determined at the IMP-8 Spacecraft 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMHK Encoder A/B Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMHK Exp A/B Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMHK Normal/Flipped Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMHK Sensor Range Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 1 1973-10-30 03:00:32 2000-05-30 12:00:11 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Geomagnetic Latitude of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Geomagnetic Longitude of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA X Geocentric SE Pos. of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Y Geocentric SE Pos. of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Z Geocentric SE Pos. of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Radial Distance Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Y Solar Magnetospheric Pos. of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Z Solar Magnetospheric Pos. of S/C Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Geomagnetic Latitude of Sun Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Geomagnetic Longitude of Sun Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA X Moon's Pos. in Geomagnetic SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Y Moon's Pos. in Geomagnetic SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Z Moon's Pos. in Geomagnetic SE Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 1 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 1 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 1 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 2 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 2 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 2 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 3 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 3 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from SE to SM, Row 3 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 1 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 1 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 1 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 2 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 2 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 2 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 3 Col 1 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 3 Col 2 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 IMP : IMP-8 : MAG_FIELD : MAG_FIELD : IMOA Rotation Matrix from CI to SE, Row 3 Col 3 Dr. James R. Sharber Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 Location of the IMP-8 Spacecraft 1 1973-10-30 02:59:00 2000-05-29 11:59:00 INTERBALL : AURORAL : OA : OA : OA Altitude INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA CGLat INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA CGLong INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA Latitude INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA Longitude INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA MLT INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA LVAL INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Vx INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Vy INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Vz INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Sun-X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Sun-Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEI Sun-Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEO X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEO Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GEO Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSE X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSE Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSE Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSM X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSM Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA GSM Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA SM X INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA SM Y INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : OA : OA : OA SM Z INTERBALL:AURORAL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Main_current INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR +5V_current INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR RAM_current INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR -12V_voltage INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR +28_voltage INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR 0V_voltage INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR +12V_voltage INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR +5V_voltage INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR DPU_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR LV-power_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Trics_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Trics_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR MEPS_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR MEPS_temp INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR ESA1 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR ESA2 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR ESA3 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CFA1 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CFA2 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CFA3 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CEM1 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CEM2 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CEM4 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR CEM3 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR ESA4 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR ESA5 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mode INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Start_azimuth INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Spin_period INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Bias_reference INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass0 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass1 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass2 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass3 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass4 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Mass5 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy0 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy1 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy2 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy3 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy4 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : MONITOR Energy5 INTERBALL:AURORAL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS Watch_dog INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS Register_overflow INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS TM_overflow INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS TC_overflow INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS Spin_simulation INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS S/W_counts INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS Test_pulses INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS ESA1 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS ESA2 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS ESA3 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS ESA4 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS ESA5 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CFA1 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CFA2 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CFA3 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CEM1 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CEM2 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CEM3 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : HK : STATUS CEM4 INTERBALL:AURORAL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:14:31 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 12_19 Electrons 169 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 12_19 Electrons 11 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 13_18 Electrons 146 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 13_18 Electrons 124 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 13_18 Electrons 56 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 13_18 Electrons 34 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 15_16 Electrons 101 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:15_16 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : MEPS : 15_16 Electrons 79 deg 0.01-35 keV INTERBALL:AURORAL:PROMICS-3:MEPS:15_16 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He2+ 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He+ 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He2+ 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He+ 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P H+ 90 deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P O+ 90 deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He2+ 90 deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P He+ 90 deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 56 amu/q 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 8 amu/q 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 56 amu/q 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 8 amu/q 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 56 amu/q deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 11P 8 amu/q deg 5-70 keV INTERBALL:AURORAL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P H+ 162 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P O+ 162 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P H+ 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P O+ 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P H+ 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P O+ 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P H+ 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10P O+ 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He2+ 162 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He+ 162 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He2+ 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He+ 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He2+ 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He+ 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He2+ 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S He+ 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 56 amu/q 162 deg <1.5keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 8 amu/q 162 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 56 amu/q 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 8 amu/q 18 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 56 amu/q 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 8 amu/q 162 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 56 amu/q 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 1__10S 8 amu/q 18 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P H+ 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P O+ 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P H+ 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P O+ 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P H+ 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P O+ 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P H+ 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9P O+ 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He2+ 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He+ 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He2+ 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He+ 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He2+ 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He+ 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He2+ 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S He+ 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 56 amu/q 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 8 amu/q 126 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 56 amu/q 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 8 amu/q 54 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 56 amu/q 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 8 amu/q 126 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 56 amu/q 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 2__9S 8 amu/q 54 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 3_8P H+ 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 3_8P O+ 90 deg <1.5 keV INTERBALL:AURORAL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 3_8P H+ 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : AURORAL : PROMICS-3 : TRICS : 3_8P O+ 90 deg 1-30 keV INTERBALL:AURORAL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1996-09-18 09:23:35 1999-01-18 06:14:47 INTERBALL : TAIL : OA : OA : OA Altitude INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA CGLat INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA CGLong INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA Latitude INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA Longitude INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA MLT INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA LVAL INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Vx INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Vy INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Vz INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Sun-X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Sun-Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEI Sun-Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEO X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEO Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GEO Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSE X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSE Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSE Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSM X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSM Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA GSM Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA SM X INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA SM Y INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : OA : OA : OA SM Z INTERBALL:TAIL:PROMICS-3:OA Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Main_current INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR +5V_current INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR RAM_current INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR -12V_voltage INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR +28_voltage INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR 0V_voltage INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR +12V_voltage INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR +5V_voltage INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR DPU_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR LV-power_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Trics_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Trics_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR MEPS_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR MEPS_temp INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR ESA1 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR ESA2 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR ESA3 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CFA1 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CFA2 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CFA3 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CEM1 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CEM2 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CEM4 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR CEM3 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR ESA4 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR ESA5 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mode INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Start_azimuth INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Spin_period INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Bias_reference INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass0 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass1 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass2 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass3 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass4 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Mass5 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy0 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy1 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy2 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy3 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy4 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : MONITOR Energy5 INTERBALL:TAIL:PROMICS-3:HK:MONITOR This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: Convert -12V_voltage from processed TM to V Uses: -0.01x TABLE 1: Convert temp form TM to Celsius Uses: (8071x-6862352)e-4 TABLE 2: Convert TM to voltage or mAmpere for sensors Uses: (x-512)*konst(TABLE3) TABLE 3: Constants for above conversion (TABLE 3) TABLE 4: Factor 1000 to convert to V from kV (HV sensors) TABLE 5: Dummy table because of bug TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS Watch_dog INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS Register_overflow INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS TM_overflow INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS TC_overflow INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS Spin_simulation INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS S/W_counts INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS Test_pulses INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS ESA1 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS ESA2 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS ESA3 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS ESA4 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS ESA5 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CFA1 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CFA2 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CFA3 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CEM1 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CEM2 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CEM3 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : HK : STATUS CEM4 INTERBALL:TAIL:PROMICS-3:HK:S/W_STATUS This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-17 10:05:36 2000-04-16 07:53:10 INTERBALL : TAIL : PROMICS-3 : MEPS : 12_19 Electrons 169 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : MEPS : 12_19 Electrons 11 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : MEPS : 13_18 Electrons 146 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion table TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : MEPS : 13_18 Electrons 124 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion table TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : MEPS : 13_18 Electrons 56 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion table TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : MEPS : 13_18 Electrons 34 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:13_18 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: table to convert count (TM) to actual numbers TABLE 2: conversion table TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : MEPS : 15_16 Electrons 101 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : MEPS : 15_16 Electrons 79 deg 0.01-35 keV INTERBALL:TAIL:PROMICS-3:MEPS:12_19 This virtual consists of two sensors from the electron spectro- meter. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: converting byte of counts to real number TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He2+ 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He+ 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He2+ 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He+ 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P H+ 90 deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P O+ 90 deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He2+ 90 deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P He+ 90 deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 56 amu/q 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 8 amu/q 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 56 amu/q 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 8 amu/q 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 56 amu/q deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 11P 8 amu/q deg 5-70 keV INTERBALL:TAIL:PROMICS-3:TRICS:S_11P This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: eflux TABLE 3: TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P H+ 162 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P O+ 162 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P H+ 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P O+ 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P H+ 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P O+ 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P H+ 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10P O+ 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: conversion from bits to counts TABLE 2: conversion constant TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He2+ 162 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He+ 162 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He2+ 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He+ 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He2+ 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He+ 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He2+ 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S He+ 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 56 amu/q 162 deg <1.5keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 8 amu/q 162 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 56 amu/q 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 8 amu/q 18 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 56 amu/q 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 8 amu/q 162 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 56 amu/q 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 1__10S 8 amu/q 18 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:1_5_6_10S This virtual consists of sensors from TRICS1, TRICS2 and TRICS3. To make conversions easier in this group of virtuals the status byte and the tables always contains entries for TRICS3 even though there are no sensors in some files from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P H+ 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P O+ 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P H+ 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P O+ 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P H+ 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P O+ 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P H+ 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9P O+ 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bits to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He2+ 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He+ 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He2+ 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He+ 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He2+ 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He+ 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He2+ 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S He+ 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 56 amu/q 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 8 amu/q 126 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 56 amu/q 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 8 amu/q 54 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 56 amu/q 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 8 amu/q 126 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 56 amu/q 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 2__9S 8 amu/q 54 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:2_4_7_9S This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-13 06:36:55 INTERBALL : TAIL : PROMICS-3 : TRICS : 3_8P H+ 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 3_8P O+ 90 deg <1.5 keV INTERBALL:TAIL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 3_8P H+ 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 INTERBALL : TAIL : PROMICS-3 : TRICS : 3_8P O+ 90 deg 1-30 keV INTERBALL:TAIL:PROMICS-3:TRICS:3_8P This virtual consists of two sensors from both TRICS1 and TRICS2. To make conversions easier in this group of virtuals the status byte and the tables also contains entries for TRICS3 even though there are nop sensor in this file from that subunit. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 2: conversion from bit to counts TABLE 3: eflux TABLE 4: TABLE 5: TABLE 6: The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-08-18 10:05:56 2000-04-16 07:57:08 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter D1 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter D2 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter D3 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter D4H This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter D4L This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter DB2 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISD Counter DB1 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G1 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G2 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G3 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G6 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G4L This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G4H This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G5L This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISG Counter G5H This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISPAG6 Pitch Angle of G6 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISS Counter S3 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISS Counter S50 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : EPD : SCIENCE : ISS Counter S80 This virtual contains all of the science parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : MAG : MAG : ISMAG Mag.Pts/Min This virtual contains all of the magnetometer parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : MAG : MAG : ISMAG Magnetic Declination This virtual contains all of the magnetometer parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : MAG : MAG : ISMAG Angle Between Spin Axis This virtual contains all of the magnetometer parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA1 Pass Number This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA1 Num First Frames This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA1 Spin Period This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA1 Local Solar Time This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA1 Local Mag. Time This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Geographic Latitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Geographic Longitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Geographic Altitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Geomagnetic Latitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Geomagnetic Longitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 Invariant Latitude This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 L This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 ISIS : ISIS-1 : OA : OA : ISOA2 B This virtual contains all of the orbit/attitude parameters for the ISIS-1 satellite Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1969-02-02 12:43:05 1969-12-29 10:52:26 MARS : MGS : MFE : ER : MGS_ELEC ER The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC Medusa The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC MTH The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC TFAS The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC 1/2TFAS The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC SPS The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_ELEC 270TH The real values are GF(rad) = 1.47 x 10**-3 cm**2 rad GF(22.5deg) = 5.76 x 10**-4 cm**2 sr dE/E = 8.24 % GF(22.5deg)dE/E = 4.75 x 10**-5 cm **2 sr dE/E dtheta = 2.2 deg DE was 6.85 x 10**-5 cm**2 sr dE/E for 10 deg. OK he gives his data in the units below(diff number flux). We need to do also diff energy flux, counts per sec and counts per accum. To get diff E flux one multiples the given number by the energy from the 18 value table converted to ergs, i.e. En(eV) x 1.6 X 10**-12 ergs/ev To get a range just use the multiply the diff N range by this factor. Now to get counts per sec multiply the diff N flux by 1.25 x 10**-3 x the energy from the table in eV. Now the counts per accum get tricky. They do 32 steps per sec and a spectra per sec. However, they do not have enough tm so they do processing on board. Note we have an 18 point spectra from them every 12 sec. For our purposes we can use our Aspera accum period (31.25 ms) which in effect normalizes the results. So multiply the above counts per sec by 31.25 ms to get counts per accum for all sensors we create, including the original ER data. MARS/MO/MFE/ER/XXXX where XXXX is derived from column 1 below and given in column 6. The last 4 virtuals {or sensors if you wish to make one virtual( which can be called electrons)} are made by multiplying the data in the ascii file for ER by column 5 values. The ER units are #/cm**2 sr eV s PGF dE/E EGF Ratio to MGS/ER Virtual 360 FOV 360 FOV cm**2 sr eV/eV cm**2 sr eV/eV MGS/ER 0.0800 0.250 0.0200 1.000 ER Medusa 0.0190 0.228 0.0043 0.215 Medusa Marty TH 0.0120 0.125 0.0015 0.076 MTH TFAS 0.0113 0.071 0.0008 0.040 TFAS 1/2 TFAS 0.00923 0.0824 0.00076 0.038 1/2TFAS DE/UARS 0.0077 0.320 0.0025 0.123 SPS 270TH 0.0444 0.06 0.0027 0.133 270TH Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:57:46 2004-04-09 10:15:08 MARS : MGS : MFE : ER : MGS_MAG Decimal Day MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Bx MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-By MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Bz MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-X MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Y MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Z MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG BTotal MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG Tip Angle MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG Clock Angle MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Bx-PC MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-By-PC MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_MAG MAG-Bz-PC MAG Data for the MARS MGS David L. Mitchell mitchell@ssl.berkeley.edu Space Sciences Laboratory http://sprg.ssl.berkeley.edu University of California Phone: 510-643-1561 Berkeley, CA 94720-7450 1 1998-03-30 12:17:31 2004-04-09 05:49:31 MARS : MGS : MFE : ER : MGS_OA SS coordinates (X) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA SS coordinates (Y) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA SS coordinates (Z) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Planetocentric coord. (X) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Planetocentric coord. (Y) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Planetocentric coord. (Z) These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA East Longitude These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Latitude These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Altitude These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Solar Zenith Angle These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : MGS : MFE : ER : MGS_OA Local Solar Time These are the OA parameters for the MARS MO. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@cluster.space.swri.edu 1 1998-03-29 12:00:00 2004-04-09 07:16:22 MARS : NOZOMI : IMI : IMI : ALPHA Sector 1 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 2 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 3 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 4 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 5 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 6 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 7 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 8 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 9 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 10 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 11 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 12 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 13 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 14 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 15 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : ALPHA Sector 16 MARS:NOZOMI:IMI:IMI:ALPHA This virtual instrument contains data from the alpha channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : EPM Sector 1 MARS:NOZOMI:IMI:IMI:EPM This virtual instrument contains data from the Energy Mass matrix, from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : EPM Sector 80 MARS:NOZOMI:IMI:IMI:EPM This virtual instrument contains data from the Energy Mass matrix, from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HEAVY Sector 1 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 2 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 3 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 4 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 5 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 6 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 7 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 8 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 9 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 10 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 11 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 12 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 13 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 14 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 15 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HEAVY Sector 16 MARS:NOZOMI:IMI:IMI:HEAVY This virtual instrument contains data from the heavy channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : HELIUM Sector 1 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 2 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 3 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 4 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 5 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 6 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 7 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 8 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 9 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 10 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 11 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 12 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 13 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 14 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 15 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HELIUM Sector 16 MARS:NOZOMI:IMI:IMI:HELIUM This virtual instrument contains data from the helium channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : HK Standby Temp MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK Bias 1 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK Bias 2 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK Post acc MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK Defl MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK 1 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK 2 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK +28i MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK F800 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : HK F801 MARS:NOZOMI:IMI:IMI:HK This virtual consists of data from NOZOMI IMI housekeeping. Olle Norberg, Masatoshi Yamauchi, ++ Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 1 1998-07-03 04:58:10 2001-07-07 10:06:46 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 1 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 2 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 3 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 4 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 5 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 6 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 7 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 8 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 9 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 10 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 11 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 12 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 13 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 14 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 15 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN Sector 16 MARS:NOZOMI:IMI:IMI:OXYGEN This virtual instrument contains data from the oxygen channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 1 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 2 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 3 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 4 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 5 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 6 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 7 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 8 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 9 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 10 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 11 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 12 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 13 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 14 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 15 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : OXYGEN2 Sector 16 MARS:NOZOMI:IMI:IMI:OXYGEN2 This virtual instrument contains data from the O2+ channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 07:35:44 1998-09-25 05:58:06 MARS : NOZOMI : IMI : IMI : PROTONS Sector 1 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 2 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 3 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 4 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 5 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 6 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 7 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 8 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 9 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 10 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 11 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 12 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 13 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 14 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 15 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : IMI : IMI : PROTONS Sector 16 MARS:NOZOMI:IMI:IMI:PROTONS This virtual instrument contains data from the proton channel from the Ion Mass Imager (IMI) instrument on the Nozomi spacecraft. The following is a list of tables which are in this vidf TABLE 0: Energy sweep table (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 My own Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 /* 00026 * Olle Norberg, Masatoshi Yamauchi, Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se, yamau@irf.se 8 1998-07-03 04:58:10 2000-03-20 04:28:21 MARS : NOZOMI : OA : OA : OA Altitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA CGLat ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA CGLong ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Latitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Longitude ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA MLT ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA L-shell ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Eclipse status ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Vx ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Vy ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Vz ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Sun-X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Sun-Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEI Sun-Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEO X ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEO Y ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA GEO Z ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA RA ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Declination ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Sun Angle ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA B-field Angle ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : NOZOMI : OA : OA : OA Spin period ASTRID:ASTRID-1:OA:OA:OA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1995-02-02 12:09:19 1995-02-28 09:52:52 MARS : PHOBOS-2 : ASPERA : ELECTRONS : PERP_HI ASPERA e- perpendicular detector D12 (0-90 deg) MARS:PHOBOS-2:ASPERA:ELECTRONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : PERP_HI ASPERA e- perpendicular detector D15 (0-90 deg) MARS:PHOBOS-2:ASPERA:ELECTRONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : PERP_HI ASPERA e- perpendicular detector D12(90-180 deg) MARS:PHOBOS-2:ASPERA:ELECTRONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : PERP_HI ASPERA e- perpendicular detector D15(90-180 deg) MARS:PHOBOS-2:ASPERA:ELECTRONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : SPECTRA ASPERA e- sunward detectors (D11+D16) MARS:PHOBOS-2:ASPERA:ELECTRONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : SPECTRA ASPERA e- perpendicular detectors (D12+D15) MARS:PHOBOS-2:ASPERA:ELECTRONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : ELECTRONS : SPECTRA ASPERA e- antisunward detectors (D13+D14) MARS:PHOBOS-2:ASPERA:ELECTRONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA H+ sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA H+ perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA H+ antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA O+ sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA O+, perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : H_O_SPEC ASPERA O+ antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:SPECTRA This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM2 sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM2 perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM2 antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM3 sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM3, perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM3 antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM4 sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM4 perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM4 antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM5 sunward detectors (D1+D10) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM5, perpendicular detectors (D3+D8) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : OTHERION ASPERA PM5 antisunward detectors (D5+D6) MARS:PHOBOS-2:ASPERA:IONS:OTHERION This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 2 1988-08-03 04:21:02 1988-08-03 04:21:02 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA H+ perpendicular detector D3 (0-90 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA H+ perpendicular detector D8 (0-90 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA H+ perpendicular detector D3 (90-180 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA H+ perpendicular detector D8 (90-180 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA O+ perpendicular detector D3 (0-90 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA O+ perpendicular detector D8 (0-90 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA O+ perpendicular detector D3 (90-180 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : ASPERA : IONS : PERP_HI ASPERA O+ perpendicular detector D8 (90-180 deg) MARS:PHOBOS-2:ASPERA:IONS:PERP_HI This virtual consists of data from the three satellite mounted electrometers. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: decompress TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2,3 0,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,0 0,4,4,4 cnts/(cm**2-str-s-eV) Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-98128 Kiruna, Sweden Olle.Norberg@irf.se 16 1988-07-25 06:21:16 1988-07-25 06:21:16 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA Bx (S/C) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA By (S/C) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA Bz (S/C) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA Btot PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA Bx (MSOR) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA By (MSOR) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : MAGMA : MAGMA : MAGMA Bz (MSOR) PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 02:51:06 1989-01-30 02:51:06 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Radial Distance PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Phi PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Theta PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT X PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Y PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Z PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Vx PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Vy PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Vz PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 MARS : PHOBOS-2 : ORBIT : ORBIT : ORBIT Vtot PHOBOS:PHOBOS-2:ORBIT:ORBIT:ORBIT This virtual consists of orbital data for PHOBOS-2 in orbit around Mars. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: 1/(detector efficiencies) TABLE 2: geometry factors (cm**2-str) TABLE 3: dE/E TABLE 4: center energies (ergs) TABLE 5: constant needed in going to dist. fn TABLE 6: (center energies)**2 (ergs**2) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,3 cnts/accum (eff. cor) Sweep 1,2 0,153 cnts/sec Sweep 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,153,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,6,7 0,153,4,4,3,4 sec**3/km**6 Olle Norberg Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1989-01-30 12:00:00 1989-01-30 12:00:00 NANOSAT : MUNIN : DINA : DINA : DINA DINA 0 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 8 2000-07-10 06:40:49 2001-01-28 11:58:47 NANOSAT : MUNIN : DINA : DINA : DINA DINA 90 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 8 2000-07-10 06:40:49 2001-01-28 11:58:47 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-4 11.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-6 33.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-8 56.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-10 78.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-12 101.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-14 123.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-15 146.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-13 168.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-2 -11.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-0 -33.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-1 -56.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-3 -78.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-5 -101.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-7 -123.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-9 -146.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSE Munin MEDUSA Electron-11 -168.75 The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@cluster.space.swri.edu 4 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-3 11.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-1 33.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-0 56.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-2 78.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-4 101.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-6 123.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-8 146.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-10 168.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-5 -11.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-7 -33.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-9 -56.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-11 -78.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-13 -101.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-15 -123.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-14 -146.25 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : MEDUSA : MEDUSA : MDSI Munin MEDUSA Ion-12 -168.75 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: sector dependent corrections The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,5 0,154,3 cor cnts/sec Sweep 1,2,3,4,5 0,154,4,4,3 cor cnts/(cm**2-str-s) Sweep 1,2,3,4,0,5 0,154,4,4,4,3cor cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,6,5 0,154,4,4,3,3cor ergs/(cm**2-str-s-eV) David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 2 2000-12-08 01:31:37 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Altitude NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA CGLat NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA CGLong NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Latitude NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Longitude NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA MLT NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA L-shell NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Eclipse status NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI X NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Y NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Z NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Vx NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Vy NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Vz NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Sun-X NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Sun-Y NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEI Sun-Z NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEO X NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEO Y NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA GEO Z NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA RA NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Declination NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Sun Angle NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA B-field Angle NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NANOSAT : MUNIN : OA : OA : OA Spin period NANOSAT:MUNIN:OA:OA:OA Rymd Plasma Gruppen Swedish Institute of Space Physics P.O. Box 812 S-981 28 Kiruna, Sweden rpg@irf.se 1 2000-12-08 09:51:08 2001-02-12 05:57:30 NOAA : NOAA-12 : MAG : MAG : N_MAG Br at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG Bt at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG Bp at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG BB at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG Br at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG Bt at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG Bp at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG BB at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_OA Geo/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_OA Geo/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_OA Geomag/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_OA Geomag/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_PA TED0 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_PA TED30 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_PA MEPED0 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_PA MEPED83 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : MAG : MAG : N_MAG_PA MEPED81 p+ Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Geo. Lat. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Geo. E. Long. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Altitude This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Magnetic Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA L-Value This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Inclination This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_OA Orbit Number This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : OA : OA : NOAA_SC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 0E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 0E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 0E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 90E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 90E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_ELEC 90E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1991-06-01 12:00:06 2002-04-30 06:02:12 NOAA : NOAA-12 : SEM : MEPED : NM_IONS 0I (6 - 55 MeV) This virtual contains all of the ION data for the NOAA/SEM/MEPED satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Ions Measured by MEPED 1 1991-06-01 12:00:00 2002-04-30 06:01:57 NOAA : NOAA-12 : SEM : MEPED : NM_IONS 90I (6 - 55 MeV) This virtual contains all of the ION data for the NOAA/SEM/MEPED satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Ions Measured by MEPED 1 1991-06-01 12:00:00 2002-04-30 06:01:57 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P6 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P6a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P6b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P7 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P7a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P7b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_OMNI P8 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 0P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 0P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 0P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 0P4 (800-2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 0P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 90P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 90P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 90P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 90P4 (800-2500 kev) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : MEPED : NM_PROT 90P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-12 : SEM : TED : NT_BK 0E-BK (elec/bkgnd) This VIDF covers the background values of the TED instrument on the NOAA satellites. TED background data are the total number of counts accumulated during the first 1/13s (background interval) on of each of the 16 energy sweeps for each of the detectors, summed, and read out once every 32 seconds. Due to the way in which the TED instrument alternates taking data between its proton and electron sensors, background data is only available to accumulate every-other sweep, thus, 16 sweeps make 32 sec even though the instrument cycle time is 1 sec. Background data are included as a quality check on the operation of the instrument. These counts generally number less than 50; if they exceed 200, possible instrument malfunctions ought to be considred. Quality values here are set to questionable when the count in an accumulation intevral exceeds values of 200 as noted above. Quality is set to bad when the TED sensor activity status flags from the telemetry stream indicate that TED is not functional. Data unknown and data state unknown are used to indicate that the data or instrument were in generating values which could not be deciphered. Background measurements are determined with no active deflection, but active sensors. The background is thus an an integral measure of the plasma rammed into the detector irrespective of what the instrument is doing. One may argu that the presence of the deflection field sweeps away the background plasma; however it can also be argued that since there is no deflection, the background represents the nutral plasma component which is uneffected by the deflection field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Electron and Proton Background Measured by TED 1 1991-06-01 12:00:29 2002-04-30 06:02:35 NOAA : NOAA-12 : SEM : TED : NT_BK 30E-BK (elec/bkgnd) This VIDF covers the background values of the TED instrument on the NOAA satellites. TED background data are the total number of counts accumulated during the first 1/13s (background interval) on of each of the 16 energy sweeps for each of the detectors, summed, and read out once every 32 seconds. Due to the way in which the TED instrument alternates taking data between its proton and electron sensors, background data is only available to accumulate every-other sweep, thus, 16 sweeps make 32 sec even though the instrument cycle time is 1 sec. Background data are included as a quality check on the operation of the instrument. These counts generally number less than 50; if they exceed 200, possible instrument malfunctions ought to be considred. Quality values here are set to questionable when the count in an accumulation intevral exceeds values of 200 as noted above. Quality is set to bad when the TED sensor activity status flags from the telemetry stream indicate that TED is not functional. Data unknown and data state unknown are used to indicate that the data or instrument were in generating values which could not be deciphered. Background measurements are determined with no active deflection, but active sensors. The background is thus an an integral measure of the plasma rammed into the detector irrespective of what the instrument is doing. One may argu that the presence of the deflection field sweeps away the background plasma; however it can also be argued that since there is no deflection, the background represents the nutral plasma component which is uneffected by the deflection field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Electron and Proton Background Measured by TED 1 1991-06-01 12:00:29 2002-04-30 06:02:35 NOAA : NOAA-12 : SEM : TED : NT_BK 0P-BK (prot/bkgnd) This VIDF covers the background values of the TED instrument on the NOAA satellites. TED background data are the total number of counts accumulated during the first 1/13s (background interval) on of each of the 16 energy sweeps for each of the detectors, summed, and read out once every 32 seconds. Due to the way in which the TED instrument alternates taking data between its proton and electron sensors, background data is only available to accumulate every-other sweep, thus, 16 sweeps make 32 sec even though the instrument cycle time is 1 sec. Background data are included as a quality check on the operation of the instrument. These counts generally number less than 50; if they exceed 200, possible instrument malfunctions ought to be considred. Quality values here are set to questionable when the count in an accumulation intevral exceeds values of 200 as noted above. Quality is set to bad when the TED sensor activity status flags from the telemetry stream indicate that TED is not functional. Data unknown and data state unknown are used to indicate that the data or instrument were in generating values which could not be deciphered. Background measurements are determined with no active deflection, but active sensors. The background is thus an an integral measure of the plasma rammed into the detector irrespective of what the instrument is doing. One may argu that the presence of the deflection field sweeps away the background plasma; however it can also be argued that since there is no deflection, the background represents the nutral plasma component which is uneffected by the deflection field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Electron and Proton Background Measured by TED 1 1991-06-01 12:00:29 2002-04-30 06:02:35 NOAA : NOAA-12 : SEM : TED : NT_BK 30P-BK (prot/bkgnd) This VIDF covers the background values of the TED instrument on the NOAA satellites. TED background data are the total number of counts accumulated during the first 1/13s (background interval) on of each of the 16 energy sweeps for each of the detectors, summed, and read out once every 32 seconds. Due to the way in which the TED instrument alternates taking data between its proton and electron sensors, background data is only available to accumulate every-other sweep, thus, 16 sweeps make 32 sec even though the instrument cycle time is 1 sec. Background data are included as a quality check on the operation of the instrument. These counts generally number less than 50; if they exceed 200, possible instrument malfunctions ought to be considred. Quality values here are set to questionable when the count in an accumulation intevral exceeds values of 200 as noted above. Quality is set to bad when the TED sensor activity status flags from the telemetry stream indicate that TED is not functional. Data unknown and data state unknown are used to indicate that the data or instrument were in generating values which could not be deciphered. Background measurements are determined with no active deflection, but active sensors. The background is thus an an integral measure of the plasma rammed into the detector irrespective of what the instrument is doing. One may argu that the presence of the deflection field sweeps away the background plasma; however it can also be argued that since there is no deflection, the background represents the nutral plasma component which is uneffected by the deflection field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Electron and Proton Background Measured by TED 1 1991-06-01 12:00:29 2002-04-30 06:02:35 NOAA : NOAA-12 : SEM : TED : NT_M 0DE Max Cnt This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 0E Max Channel This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 30DE Max Cnt This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 30E Max Channel This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 0DP Max Cnt This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 0P Max Channel This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 30DP Max Cnt This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_M 30P Max Channel This VIDF contains the counts obtained for the maximum energy channel and the energy channel receiving that maximum for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0EF-D Flux This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0DE Max Cnt This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0E Max Channel This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30EF-D Flux This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30DE Max Cnt This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30E Max Channel This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0PF-D Flux This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0DP Max Cnt This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 0D Max Channel This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30PF-D Flux This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30DP Max Cnt This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S1 30P Max Channel This VIDF covers the science data of the TED instrument on the NOAA satellites. It contains the total flux obtained from each sensor sweep and the maximum for that sweep. The maximum energy channel accumulation and the energy channel receiving that maximum is included in the data set for the TED instrument on the NOAA satellites. Table 0 is used as a dummy table to send the idf stored value into the data buffer where it can be manipulated. Table 1 is the accumulation rate for one sample. Warning, the data accumulation time is the entire sweep eventhough the data which is represented only comes from one step (1-11) of that sweep. Table 2 then converts the count rate into the differential directional energy flux. Table 3 represents the center energy of the channel, Table 4 and Table 5 are the lower and upper energy limits of the channel. Table 6 represents the altitude where NOAA believes that the energy from the channel falls in the atmosphere. Table 7 is the individual conversion rates for each energy channel. The conversion factors convert count to directional energy flux. Table 8 contains the conversion factor to convert the count to directional energy flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Maximum Electron and Proton Flux Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d e- Channel 1 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d e- Channel 3 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d e- Channel 5 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d e- Channel 7 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d e- Channel 1 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d e- Channel 3 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d e- Channel 5 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d e- Channel 7 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d p+ Channel 1 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d p+ Channel 3 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d p+ Channel 5 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 0d p+ Channel 7 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d p+ Channel 1 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d p+ Channel 3 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d p+ Channel 5 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : NT_S2 30d p+ Channel 7 This VIDF covers the science sensors of the TED instrument on the NOAA satellites. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Routine Electron and Proton Values Measured by TED 1 1991-06-01 12:00:05 2002-04-30 06:02:11 NOAA : NOAA-12 : SEM : TED : TEDFX TED Full Energy Flux This VIDF covers the TED Full Energy Flux of the TED instrument on the NOAA satellites. The value of the Full energy flux is a derived quantity by ground data processing. Full Energy Flux is computed every two seconds using both proton and electron sensors. If neither of the two detector pairs is viewing charged particles that reach the Earth's atmosphere, then the value of the Total Energy Flux is set to 0. The situation in which neither detector pair views charged particles that can reach the atmosphere is confined to measurements made at rather low geographic latitudes, where any energy flow into the atmosphere is expected to be small. Whenever bad data were identified within a 2-second data record, the corresponding entry for the total energy flux is set to 1000 mW/m**2 (an energy flux beyond the maximum that could be detected by the instrument). The largest possible valid total energy flux value is approx- imately 600 mW/m**2. The smallest value is approximately 0.001 mW/m**2. A value of total energy flux of 995 mW/m**2 indicates that TED was not operating in its normal operational mode. Quality values of 1 indicate that the TED value is greater than 600 and should the data should be questioned. Quality values of 2 or higher indicate that the data was invalid. Quality value reflected is the worst quality seen within the number of samples of the sensor recorded within the data record. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Low-Energy Full Energy Flux Measured by TED 1 1991-06-01 12:00:07 2002-04-30 06:02:13 NOAA : NOAA-15 : MAG : MAG : N_MAG Br at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG Bt at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG Bp at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG BB at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG Br at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG Bt at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG Bp at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG BB at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_OA Geo/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_OA Geo/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_OA Geomag/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_OA Geomag/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_PA TED0 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_PA TED30 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_PA MEPED0 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_PA MEPED83 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : MAG : MAG : N_MAG_PA MEPED81 p+ Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Geo. Lat. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Geo. E. Long. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Altitude This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Magnetic Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA L-Value This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Inclination This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_OA Orbit Number This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : OA : OA : NOAA_SC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 1998-07-01 12:00:14 2007-11-05 12:00:04 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 0E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 0E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 0E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 90E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 90E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_ELEC 90E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 1998-07-01 12:00:13 2007-11-05 07:09:31 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P6 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P6a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P6b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P7 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P7a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P7b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_OMNI P8 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 1998-07-01 12:00:12 2007-11-05 04:50:10 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 0P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 0P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 0P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 0P4 (800-2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 0P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 90P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 90P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 90P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 90P4 (800-2500 kev) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-15 : SEM : MEPED : NM_PROT 90P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. This virtual contains the proton data from MEPED. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. The proton data contains two sensors, one mounted at 0 deg in the zenith direction, and the other mounted at 90 deg, in the ram direction. Each proton sensor has 5 pass bands. Data is stored in this IDFS as counts per accumulation. A dummy Table 0 is provided to put these counts into the working buffer so that it may be turned into a count rate by dividing by the accumulation time (Table 0, operation 150), giving counts per sec. Dividing counts per sec (operation 4) by the geometric factor (stored in Table 1) gives the counts/(cm^2 sr s), or number flux. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 1998-07-01 12:00:14 2007-11-05 12:20:52 NOAA : NOAA-16 : MAG : MAG : N_MAG Br at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG Bt at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG Bp at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG BB at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG Br at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG Bt at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG Bp at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG BB at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_OA Geo/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_OA Geo/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_OA Geomag/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_OA Geomag/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_PA TED0 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_PA TED30 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_PA MEPED0 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_PA MEPED83 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : MAG : MAG : N_MAG_PA MEPED81 p+ Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Geo. Lat. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Geo. E. Long. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Altitude This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Magnetic Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA L-Value This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Inclination This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_OA Orbit Number This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : OA : OA : NOAA_SC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2001-01-10 12:00:27 2007-11-05 12:00:31 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 0E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 0E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 0E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 90E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 90E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_ELEC 90E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2001-01-10 12:00:26 2007-11-05 07:09:58 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P6 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P6a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P6b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P7 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P7a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P7b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_OMNI P8 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2001-01-10 12:00:25 2007-11-05 04:50:37 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 0P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 0P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 0P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 0P4 (800-2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 0P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 90P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 90P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 90P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 90P4 (800-2500 kev) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-16 : SEM : MEPED : NM_PROT 90P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2001-01-10 12:00:27 2007-11-05 12:21:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Br at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Bt at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Bp at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG BB at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Br at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Bt at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG Bp at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG BB at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_OA Geo/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_OA Geo/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_OA Geomag/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_OA Geomag/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_PA TED0 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_PA TED30 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_PA MEPED0 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_PA MEPED83 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : MAG : MAG : N_MAG_PA MEPED81 p+ Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Geo. Lat. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Geo. E. Long. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Altitude This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Magnetic Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA L-Value This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Inclination This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_OA Orbit Number This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : OA : OA : NOAA_SC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2002-07-12 12:54:22 2007-11-05 12:00:19 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 0E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 0E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 0E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 90E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 90E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_ELEC 90E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2002-07-12 12:54:21 2007-11-05 07:09:46 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P6 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P6a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P6b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P7 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P7a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P7b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_OMNI P8 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2002-07-12 12:54:20 2007-11-05 04:50:25 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 0P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 0P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 0P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 0P4 (800-2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 0P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 90P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 90P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 90P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 90P4 (800-2500 kev) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-17 : SEM : MEPED : NM_PROT 90P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2002-07-12 12:54:22 2007-11-05 12:21:07 NOAA : NOAA-18 : MAG : MAG : N_MAG Br at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG Bt at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG Bp at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG BB at Satellite This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG Br at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG Bt at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG Bp at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG BB at FOFL This virtual contains all of the magnetometer data parameters for the NOAA/SEM satellite. Magnetic field values are given in terms of spherical coordinates and represent the field in nT. Two sets are given, those at the spacecraft and another set at the 120 km altitude level (defined as the top of the atmosphere and the Foot Of the Field Line - FOFL). Spherical coordinates are computed from a magnetic field model and given as the radial, theta, and phi components, and the total magnitude of the field. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 Earth's Magnetic Field for the NOAA Spacecraft 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_OA Geo/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_OA Geo/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_OA Geomag/Lat/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_OA Geomag/East Long/FOFL This virtual contains all of the orbit/attitude parameters for the NOAA/SEM satellite determined by the mapping of the magnetic field. Basically, the magnetic field line is traced down to 120 km. The 120 km value is assumed to be the top of the atmosphere and also called the Foot Of the Field Line (FOFL). This virtual contains the geographic and geometic locations of the FOFL traced from the spacecraft position. Positions values are in degrees. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Position of the Magnetic Foot of the Field Line on the Earth 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_PA TED0 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_PA TED30 Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_PA MEPED0 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_PA MEPED83 e- Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : MAG : MAG : N_MAG_PA MEPED81 p+ Pitch Angle This virtual contains all of the pitch angle parameters for the NOAA/SEM satellite. Pitch angle valies are given in degrees. The TED pitch angles are computed at the 120 km level (also defined as the top of the atmosphere or the Foot Of the Field Line - FOFL). The MEPED pitch angles are determined at the spacecraft. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Pitch Angle for the TED and MEPED 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Geo. Lat. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Geo. E. Long. This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Altitude This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Magnetic Local Time This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA L-Value This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Inclination This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_OA Orbit Number This virtual contains all of the orbit/attitude parameters for the NOAA satellite Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geographic and Other Orbital Parameters 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Geocentric Latitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Geocentric Longitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Geocentric Altitude Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Staciewicz Cor/Geomag/Long Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Staciewicz Cor/Mag/Local Time Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Staciewicz Cor/Invar/Lat Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : OA : OA : NOAA_SC Staciewicz Cor/L-Shell Value Stasiewicz values are determined from the Geographic positions of the spacecraft within the O/A data as if they were exact to 0.1 Degree. The computed values included within this data set are as follows: Sensor Sensor Name IDF units Number 0 Geocentric Latitude degrees 1 Geocentric Longitude degrees 2 Geocentric Altitude kilometers 3 Stasiewicz Corrected Geomagnetic Latitude degrees 4 Stasiewicz Corrected Geomagnetic Longitude degrees 5 Stasiewicz Corrected Magnetic Local Time hours 6 Stasiewicz Corrected Invariant Latitude degrees 7 Stasiewicz Corrected L-Shell Value unitless Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA Geocentric and Stasiewicz Corrected Orbit Data 1 2005-06-07 12:00:07 2007-11-05 12:00:04 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 0E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 0E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 0E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 90E1 (> 30 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 90E2 (> 100 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_ELEC 90E3 (> 300 keV) This virtual contains all of the sensors for the the NOAA/SEM/MEPED electron sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The electron detector is a thin 25 mm**2 solid-state detector covered by 0.51 um thick nickel foil (0.70 um in the case of TIROS-N), that suppresses detector response to photons and reduces pulse pile-up caused by incident low-energy electrons or ions. Electronic pulse-height discrimination is used to select pules due to incident electrons of nominal energies greater than 30 keV, 100 keV, and 300 keV (taking into account a nominal 5 keV energy loss as the electron passes through the foil). The contaminant response to protons that deposit more than 1 MeV in the detector is eliminated electronically. The detectors are, however, sensitive to protons between about 135 keV and 1 MeV. Data from the directional proton detectors may be used to correct for this effect. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Electrons Measured by MEPED 1 2005-06-07 12:00:06 2007-11-05 07:10:35 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P6 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P6a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P6b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P7 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P7a This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P7b This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_OMNI P8 This virtual contains all of the sensors for the the NOAA/SEM/MEPED omni-directional proton sensors The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The telescopes are mounted in two pairs, one of pair detecting electrons, the other detecting protons (and heavier ions). One pair of detectors is mounted to view outward along the Earth-satellite radial vector zenith. At geomagnetic latitudes greater than 30 degrees, these detectors view charged particles that are in the atmospheric loss cone and will enter the atmosphere. The other detector pair is mounted to view at about 80 degrees to the first, and for magnetic latitudes greater than 30 degrees will measure particles that have pitch angles near 90 degrees (i.e. particles that are outside the loss cone are trapped). For convenience, these two detectors are identified with the prefix 0 and 90. The local pitch angles of the particles observed by these two pairs of directional detectors at any point in the orbit are calculated using a model magentic field developed at the NSSDC (Stassinopolis and Mead, 1972). The pitch angle data is available as a separate virtual. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Omni Measured Particles by MEPED 1 2005-06-07 12:00:05 2007-11-05 04:50:10 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 0P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 0P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 0P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 0P4 (800-2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 0P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 90P1 (30-80 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 90P2 (80-250 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 90P3 (250-800 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 90P4 (800-2500 kev) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 NOAA : NOAA-18 : SEM : MEPED : NM_PROT 90P5 (> 2500 keV) This virtual contains all of the PROTON data for the NOAA/SEM satellite The MEPED (Medium Energy Proton and Electron Detector) is that portion of the SEM designed to measure the flux of protons (ions) and electrons mirroring above, and precipitating into, the high-latitude atmosphere. Each MEPED consists of two sensor assemblies: the directional (telescope) particle detectors and the omnidirectional proton detectors. The proton (ion) detector within each telescope is a two-element, solid-state detector telescope. The front element has an effective area of 25 mm**2 and thickness of 200 um. The back element has an effective area of 50 mm**2 and a thickness of 200 um. A 2500-gauss magnet is mounted across the input aperture of this detector assembly to prevent any electrons of energies less than 1.5 MeV from reaching the detectors. The front face of the front detector of the telescope is coated with an aluminum layer 18ug cm**-2 thick, which serves both as an electrical contact and a suppressor of the detector's sensitivity to photons. Dr. Janet Green NOAA E16C2 325 Broadway Boulder, CO 80303 (303) 497-4845 NOAA High-Energy Protons Measured by MEPED 1 2005-06-07 12:00:07 2007-11-05 12:20:52 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Bx PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED By PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Bz PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Btot PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED DIN PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Pitch(1) PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Pitch(2) PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED IQF PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED ID PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Monitor PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED Integral Flux PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D1a PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D2a PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D3 PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D4 PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D1b PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D2b PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D5 PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : MAG : MAG : MERGED D6 PROGNOZ:PROGNOZ-7:MAG:MAG:MERGED This virtual consists of merged data from the satellite magnetometers, picth angles and detectors There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-11-02 09:49:26 1979-05-25 09:46:27 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT Height PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT Lat PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT Long PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT TGM PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT TA PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT TS PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT B PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT L PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT BR PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT BT PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT BF PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT Ecclipse PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SE R PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SE lat PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SE long PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GM lat PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GM long PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GSM x PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GSM y PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GSM z PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GSM lat PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT GSM long PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SM x PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SM y PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SM z PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SM lat PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : ORBIT : ORBIT : ORBIT SM long PROGNOZ:PROGNOZ-7:ORBIT:ORBIT:ORBIT This virtual consists of orbit data from the satellite There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 1 1978-10-30 06:45:50 1979-01-01 12:47:06 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 2.14 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 2.89 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 3.89 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 5.23 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 7.04 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 9.40 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 12.7 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D1 D1 16.9 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D1 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 2-16 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.20 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.27 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.36 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.48 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.65 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 0.87 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 1.17 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D2 D2 1.57 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D2 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.34-1.1 keV. The conversion factor is xxx and the field of view yyy deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D3 D3 perp. ion spectrometer PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D3 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 90 deg. from the spin axis and has an energy range of 0.02-30 keV. The conversion factor is 1.09e-4 and the field of view 5x13 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 4 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 0.65 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 0.87 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 1.17 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 1.57 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 2.12 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 2.83 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 3.80 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 PROGNOZ : PROGNOZ-7 : PROMICS-1 : PROMICS-1 : D6 D6 5.08 keV PROGNOZ:PROGNOZ-7:PROMICS-1:PROMICS-1:D6 This virtual consists of data from the one of satellite ion spectrometers. The detector is mounted 25 deg. from the spin axis and has an energy range of 0.61-4.88 keV. The conversion factor is 5.31e-5 and the field of view 5x6 deg. There will be a desc of tables when they are included. Ulrik Eklund Swedish Institute of Space Physics P.O. Box 812 S-981 28 KIRUNA, Sweden E-mail: ulrik@irf.se 32 1978-11-02 09:50:58 1979-04-02 02:45:49 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID H+ Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID He+ Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID He++ Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID O+ Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID O++ Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOID Total Ion Density This is the data base of number densities for H+, He+, He++, O+, O++, and total Ions that Martin Wuest generated for Richard Denton. The values are stored as floats in units of #/cm**3. Dr. Martin Wuest Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Martin.Wuest@inficon.com Wuest Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 01:28:28 1991-08-20 12:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD H+ Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD He+ Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD He++ Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD O+ Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD O++ Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOKD Total Ion Density * This is the data base of number densities for H+, He+, He++, O+, O++, * and total Ions that SwRI generated for Richard Denton. The values are * stored as floats in units of #/cm**3. Dr. Rudy Frahm Space Science Dept./Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA e-mail: Rfrahm@swri.edu SwRI Densities of H+, He+, He++, O+, O++, and total Ions from CRRES LOMICS 1 1990-08-26 08:36:21 1991-08-20 12:00:44 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN Other * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN H'sup +' * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN He'sup 2+ ' * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN He'sup +' * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN O'sup 2+' * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN O'sup +' * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 0, Heavy Ions * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 1, Light Ions * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 2, Start Counts from TOF * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 3, Start Counts ID=0 * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 4, Start Counts ID=1 * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 5, Start Counts ID=2 * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN Other Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN H'sup +' Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN He'sup 2+' Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN He'sup +' Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN O'sup 2+' Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN O'sup +' Threshold * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 0, Heavy Ions Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 1, Light Ions Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 2, TOF Start Counts Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 3, Start Counts ID=0 Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 4, Start Counts ID=1 Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMN LS Scalar 5, Start Counts ID=2 Thresh * The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), * one of the SPACERAD instruments on CRRES, * is a time-of-flight mass spectrometer designed to distinguish * and measure the velocity distributions of all important * magnetospheric ion species up to 44 keV per charge. * * Azimuthal zero degree position of the spacecraft x-axis * corresponds to view most nearly along the geographic North pole (ZGEI). * * The instrument has problems with sagging of the TOF high voltage supply. * * The following table shows which units can be obtained and which tables * (in physical order) have to be applied. * * unit table(s) * ------------------------------------------------------------------------- * energy/charge eV/q 0 * energy eV 0,2 * countrate counts/sec 3 * modified number flux counts/(sec cm2 sr) 3,4 * modified number flux/(dE/E) counts/(sec cm2 sr) 3,4,5 * differential number flux counts/(sec cm2 sr ev) 3,4,5,6 * distribution function sec3/km6 3,4,5,7,8 * ------------------------------------------------------------------------- * * References: * * CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, * R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force * Geophysics Laboratory, Hanscom AFB, 24.0 January 1985 * * CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and * S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, * Los Angeles, CA 90009, July 1990 * * The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), * D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, * R. Vigil, J. Spacecraft and Rockets, Sept. (19992) * Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES LOMICS Ion Fluxes between 100 eV and 44 keV 32 1990-08-26 08:36:21 1993-08-26 09:01:05 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMQ ID0 The Low Energy Magnetospheric IOn Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 4 1990-08-26 08:36:21 1991-08-20 02:42:23 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMQ ID1 The Low Energy Magnetospheric IOn Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 4 1990-08-26 08:36:21 1991-08-20 02:42:23 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMQ ID2 The Low Energy Magnetospheric IOn Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 4 1990-08-26 08:36:21 1991-08-20 02:42:23 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMQ ID3 (forbidden) The Low Energy Magnetospheric IOn Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 4 1990-08-26 08:36:21 1991-08-20 02:42:23 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMS Time-of-Flight The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force Geophysics Laboratory, Hanscom AFB, 24. January 1985 CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, Los Angeles, CA 90009, July 1990 The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, R. Vigil, J. Spacecraft and Rockets, 29, 596, Sept. (1992) Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 1536 1990-08-26 10:01:33 1991-08-02 05:07:50 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMS ID The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force Geophysics Laboratory, Hanscom AFB, 24. January 1985 CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, Los Angeles, CA 90009, July 1990 The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, R. Vigil, J. Spacecraft and Rockets, 29, 596, Sept. (1992) Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 1536 1990-08-26 10:01:33 1991-08-02 05:07:50 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMS E/Q The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force Geophysics Laboratory, Hanscom AFB, 24. January 1985 CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, Los Angeles, CA 90009, July 1990 The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, R. Vigil, J. Spacecraft and Rockets, 29, 596, Sept. (1992) Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 1536 1990-08-26 10:01:33 1991-08-02 05:07:50 SPACERAD : CRRES : AFGL-701-11 : LOMICS : LOMS M/Q The Low Energy Magnetospheric Ion Composition Sensor (LOMICS), one of the SPACERAD instruments on CRRES, is a time-of-flight mass spectrometer designed to distinguish and measure the velocity distributions of all important magnetospheric ion species up to 44 keV per charge. Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). The instrument has problems with sagging of the TOF high voltage supply. References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL Technical Report, AFGL-TR-85-0017, Air Force Geophysics Laboratory, Hanscom AFB, 24. January 1985 CRRES AFGL-701-11B (DPUB/HMSB) Experiment Handbook, R.Koga and S.D. Pinkerton, Space Sciences Laboratory, The Aerospace Corporation, Los Angeles, CA 90009, July 1990 The CRRES Low-Energy Magnetospheric Ion Composition Sensor (LOMICS), D.T. Young, B.L. Barraclough, D.J. McComas, M.F. Thomsen, K. McCabe, R. Vigil, J. Spacecraft and Rockets, 29, 596, Sept. (1992) Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA 1536 1990-08-26 10:01:33 1991-08-02 05:07:50 SPACERAD : CRRES : AFGL-701-13-1 : MAG : BMAG Bx A Schonstedt Instrument Company triaxial fluxgate magnetometer which samples each axis on two different ranges +/- 45000 nT and +/- 1000 nT. The fluxgate magnetometer sensor is mounted on a boom, 6.1m in length, in order to get it far enough away from the spacecraft body, so that the total vehicle generated magnetic field will have a strength less than 2 nT at the sensor location along the spin axis and 4 nT in the spin plane. The three axes of the magnetometer are mutually orthogonal to approximately 0.08 deg. The Earth's magnetic field is measured 16 times per second, but only 8 values per second are written to the distributed agency tape. Calibration is done using the MAGMEM5.FOR algorithm available on the AFGL VAX Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL TechnicalReport, AFGL-TR-85-0017, 24 January 1985 CRRES Agency Tape Generation, A.R.Griffin,D.E. Delorey,R.E.McInerney, GL Technical Memorandum No. 174, Hanscom AFB, 1989 Fluxgate Magnetometer Instrument on the Combined Release and Radiation Effects Satellite (CRRES), H.J. Singer,W.P. Sullivan,P.Anderson, F.Mozer,P.Harvew,J.Wygant,W.McNeil, J. Spacecraft and Rockets, Sept.(1992) On-line documentation on SPAN directory AFGLSC::USER3:[PH.CRRES.README.MAGFILE] Dr. Howard J. Singer Air Force Geophysics Laboratory Hanscom AFB, MA 01731 32 1990-08-24 07:41:02 1991-08-20 02:41:05 SPACERAD : CRRES : AFGL-701-13-1 : MAG : BMAG By A Schonstedt Instrument Company triaxial fluxgate magnetometer which samples each axis on two different ranges +/- 45000 nT and +/- 1000 nT. The fluxgate magnetometer sensor is mounted on a boom, 6.1m in length, in order to get it far enough away from the spacecraft body, so that the total vehicle generated magnetic field will have a strength less than 2 nT at the sensor location along the spin axis and 4 nT in the spin plane. The three axes of the magnetometer are mutually orthogonal to approximately 0.08 deg. The Earth's magnetic field is measured 16 times per second, but only 8 values per second are written to the distributed agency tape. Calibration is done using the MAGMEM5.FOR algorithm available on the AFGL VAX Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL TechnicalReport, AFGL-TR-85-0017, 24 January 1985 CRRES Agency Tape Generation, A.R.Griffin,D.E. Delorey,R.E.McInerney, GL Technical Memorandum No. 174, Hanscom AFB, 1989 Fluxgate Magnetometer Instrument on the Combined Release and Radiation Effects Satellite (CRRES), H.J. Singer,W.P. Sullivan,P.Anderson, F.Mozer,P.Harvew,J.Wygant,W.McNeil, J. Spacecraft and Rockets, Sept.(1992) On-line documentation on SPAN directory AFGLSC::USER3:[PH.CRRES.README.MAGFILE] Dr. Howard J. Singer Air Force Geophysics Laboratory Hanscom AFB, MA 01731 32 1990-08-24 07:41:02 1991-08-20 02:41:05 SPACERAD : CRRES : AFGL-701-13-1 : MAG : BMAG Bz A Schonstedt Instrument Company triaxial fluxgate magnetometer which samples each axis on two different ranges +/- 45000 nT and +/- 1000 nT. The fluxgate magnetometer sensor is mounted on a boom, 6.1m in length, in order to get it far enough away from the spacecraft body, so that the total vehicle generated magnetic field will have a strength less than 2 nT at the sensor location along the spin axis and 4 nT in the spin plane. The three axes of the magnetometer are mutually orthogonal to approximately 0.08 deg. The Earth's magnetic field is measured 16 times per second, but only 8 values per second are written to the distributed agency tape. Calibration is done using the MAGMEM5.FOR algorithm available on the AFGL VAX Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL TechnicalReport, AFGL-TR-85-0017, 24 January 1985 CRRES Agency Tape Generation, A.R.Griffin,D.E. Delorey,R.E.McInerney, GL Technical Memorandum No. 174, Hanscom AFB, 1989 Fluxgate Magnetometer Instrument on the Combined Release and Radiation Effects Satellite (CRRES), H.J. Singer,W.P. Sullivan,P.Anderson, F.Mozer,P.Harvew,J.Wygant,W.McNeil, J. Spacecraft and Rockets, Sept.(1992) On-line documentation on SPAN directory AFGLSC::USER3:[PH.CRRES.README.MAGFILE] Dr. Howard J. Singer Air Force Geophysics Laboratory Hanscom AFB, MA 01731 32 1990-08-24 07:41:02 1991-08-20 02:41:05 SPACERAD : CRRES : AFGL-701-13-1 : MAG : BMAG |B| A Schonstedt Instrument Company triaxial fluxgate magnetometer which samples each axis on two different ranges +/- 45000 nT and +/- 1000 nT. The fluxgate magnetometer sensor is mounted on a boom, 6.1m in length, in order to get it far enough away from the spacecraft body, so that the total vehicle generated magnetic field will have a strength less than 2 nT at the sensor location along the spin axis and 4 nT in the spin plane. The three axes of the magnetometer are mutually orthogonal to approximately 0.08 deg. The Earth's magnetic field is measured 16 times per second, but only 8 values per second are written to the distributed agency tape. Calibration is done using the MAGMEM5.FOR algorithm available on the AFGL VAX Azimuthal zero degree position of the spacecraft x-axis corresponds to view most nearly along the geographic North pole (ZGEI). References: CRRES/SPACERAD Experiment Descriptions, M.S. Gussenhoven,E.G. Mullen, R.C. Sagalyn, Eds., AFGL TechnicalReport, AFGL-TR-85-0017, 24 January 1985 CRRES Agency Tape Generation, A.R.Griffin,D.E. Delorey,R.E.McInerney, GL Technical Memorandum No. 174, Hanscom AFB, 1989 Fluxgate Magnetometer Instrument on the Combined Release and Radiation Effects Satellite (CRRES), H.J. Singer,W.P. Sullivan,P.Anderson, F.Mozer,P.Harvew,J.Wygant,W.McNeil, J. Spacecraft and Rockets, Sept.(1992) On-line documentation on SPAN directory AFGLSC::USER3:[PH.CRRES.README.MAGFILE] Dr. Howard J. Singer Air Force Geophysics Laboratory Hanscom AFB, MA 01731 32 1990-08-24 07:41:02 1991-08-20 02:41:05 SPACERAD : CRRES : AFGL-701-13-1 : MAG : PANG Pitch Angle The pitch angle is calculated from the CRRES AFGL-701-13-1 Fluxgate magnetometer. The magnetic field in spacecraft coordinates is taken and the angle to the negative x-axis (look direction of the LOMICS plasma sensor) is calculated. The pitch angle is in degrees. Dr. Howard J. Singer Air Force Geophysics Laboratory Hanscom AFB, MA 01731 32 1990-08-26 08:59:00 1991-08-06 04:49:02 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Julian Date (days) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE UT (sec) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE X ECI Satellite Position Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Y ECI Satellite Postion Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Z ECI Satellite Position Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Vx ECI Satellite Velocity Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Vy ECI Satellite Velocity Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Vz ECI Satellite Velocity Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Satellite Radius Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Satellite Altitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Satellite Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Satellite Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Satellite Velocity Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Geoc Local Time Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Mag. Radius Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Mag. Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Mag. Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE SM Radius Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE SM Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE SM Local Time Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE GSM Radius Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE GSM Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE GSM Local Time Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B (model) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bx (ECI) Olson-Pfitzer model Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE By (ECI, model) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bz (ECI, model) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE MLT Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Solar Zenith Angle Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Invariant Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100N Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100N Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100S Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100S Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE L-Shell Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bmin Mag. Field Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bmin Geoc. Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bmin Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bmin Altitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bconj Latitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bconj Longitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Bconj Altitude Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Sun position X (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Sun position Y (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Sun position Z (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Moon position X (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Moon position Y (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Moon position Z (ECI) Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Right Ascension of Greenwich Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100s mag field Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE B100n mag field Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole moment MX ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole moment MY ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole moment MZ ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole offset MX ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole offset MY ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SPACERAD : CRRES : EPHEMERIS : EPHEM : EPHE Dipole offset MZ ECI Ephemeris data of the CRRES satellite Dr. Dave T. Young Space Science Dept. Southwest Research Instiute P.O. Drawer 28510 San Antonio, Texas 78228-0510, USA CRRES Ephemeris Data 1 1990-08-24 09:49:00 1991-08-19 04:41:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MERCURY to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP VENUS to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP EARTH to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP MARS to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP JUPITER to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP SATURN to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP URANUS to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to PLUTO Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP NEPTUNE to PLUTO Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO X Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Y Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Z Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO R Magnitude Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Theta Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Phi Position Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO X Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Y Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Z Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO R Magnitude Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Theta Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO Phi Velocity Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to MERCURY Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to VENUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to EARTH Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to MARS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to JUPITER Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to SATURN Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to URANUS Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to NEPTUNE Separation Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to MERCURY Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to VENUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to EARTH Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to MARS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to JUPITER Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to SATURN Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to URANUS Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 SUN : Solar_System : Planets : Orientation : SUNPP PLUTO to NEPTUNE Projection Barycenter * This virtual contains the position and orbital velocity for each planet * (Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, and Pluto) * about the Solar System Barycenter. Also computed is the angle between * each planet and the angular difference between the projection of each * planet's position on the Solar System Barycenter equitorial plane (positive * angles means that the secondary planet leads the primary planet, negative * angles meanthat the secondary planet lags the primary planet). * * Since the objects are considered to be moving with respect to the Solar * System Barycenter, their quantities vary with time. Each object produces * 28 quantities. They are as follows for each object: * * SENSOR ORDER QUANTITY STORAGE UNIT MEANING * 0 + n X km Barycenteric X position * 1 + n Y km Barycenteric Y position * 2 + n Z km Barycenteric Z position * 3 + n R km Barycenteric R position * 4 + n T km Barycenteric Theta position angle * 5 + n P km Barycenteric Phi position angle * 6 + n VX km/sec Barycenteric X velocity * 7 + n VX km/sec Barycenteric Y velocity * 8 + n VX km/sec Barycenteric Z velocity * 9 + n VR km/sec Barycenteric R velocity * 10 + n VT km/sec Barycenteric Theta velocity angle * 11 + n VP km/sec Barycenteric Phi velocity angle * 12 + n n_A_1 degrees Angle to 1st secondary planet * 13 + n n_A_2 degrees Angle to 2nd secondary planet * 14 + n n_A_3 degrees Angle to 3rd secondary planet * 15 + n n_A_4 degrees Angle to 4th secondary planet * 16 + n n_A_5 degrees Angle to 5th secondary planet * 17 + n n_A_6 degrees Angle to 6th secondary planet * 18 + n n_A_7 degrees Angle to 7th secondary planet * 19 + n n_A_8 degrees Angle to 8th secondary planet * 20 + n n_P_1 degrees Project Angle to 1st secondary planet * 21 + n n_P_2 degrees Project Angle to 2nd secondary planet * 22 + n n_P_3 degrees Project Angle to 3rd secondary planet * 23 + n n_P_4 degrees Project Angle to 4th secondary planet * 24 + n n_P_5 degrees Project Angle to 5th secondary planet * 25 + n n_P_6 degrees Project Angle to 6th secondary planet * 26 + n n_P_7 degrees Project Angle to 7th secondary planet * 27 + n n_P_8 degrees Project Angle to 8th secondary planet * * where n = Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, Neptune, * Pluto * * The following is a list of tables which are in this vidf: * TABLE 0: Polynomial coefficients for converting values stored * in km or km/sec into m or m/sec * TABLE 1: Polynomial coefficients for converting values stored * in km or km/sec into cm or cm/sec * TABLE 2: Polynomial coefficients for converting values stored * in km or km/sec into AU or AU/sec * * Data is stored in km for distance measures, km/sec for velocities, * and degrees for angles. The following are units which can be * derived from the tables. The format is to give the tables applied * followed by the operations and unit definition: * * DATA TYPE TABLES OPERS UNIT * Sensor 0 0 m or m/sec * Sensor 1 0 cm or cm/sec * Sensor 2 0 AU or AU/sec 1 1901-01-01 12:00:00 2010-12-31 12:00:00 TSS : TSS-1 : CAS : CAS : CSAA IMU Body Rate X TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA IMU Body Rate Y TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA IMU Body Rate Z TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Q-M50 To Body Ele1 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Q-M50 To Body Ele2 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Q-M50 To Body Ele3 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Q-M50 To Body Ele4 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Q-M50 To Body Time TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA M50 (LV,LH) Q1 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA M50 (LV,LH) Q2 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA M50 (LV,LH) Q3 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA M50 (LV,LH) Q4 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Roll Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Pitch Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Yaw Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Shuttle Alt TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Cur Apogee TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAA Cur Perigee TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur XPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur YPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur ZPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur XVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur YVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Fltrs Cur ZVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target XPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target YPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target ZPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target XVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target YVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Cur Target ZVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Target XAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Target YAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Target ZAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar XPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar YPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar ZPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar XVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar YVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Rel Orb/Tar ZVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Last Tar Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Last State Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSAB Filter State Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Shuttle Lat TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Shuttle Long TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Pitch (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Yaw (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Roll (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Pitch Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Yaw Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Roll Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Sat Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Sat Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Ram Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Ram Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCA Orbit # TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCB FES Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCB Water Dump Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSCB Thruster Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS LT BL T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS RT BL T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS LT BL T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS RT BL T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS L Sill Longn T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS L Sill Longn T@1030 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS L Sill Longn T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS R Sill Longn T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS R Sill Longn T@1030 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA M-FUS R Sill Longn T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 1 Evap Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 2 Evap Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 1 Rad Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 2 Rad Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 1 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 2 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 3 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 1 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 2 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA FCL 3 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA Mid PCA Main Bus A I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA Mid PCA Main Bus B I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA P/L Pri Main Bus B V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEA P/L Pri Main Bus C V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEB Sup H2O Tank A Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEB Sup H2O Tank B Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEB Sup H2O Tank C Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEB Sup H2O Tank D Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSEB Waste H2O Tank Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 Roll Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 Pitch Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 DES Roll Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 DES Pitch Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 Rng Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 Roll Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMA KU-A CH1 Pitch Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMB KU-A CH1 Radar Rng TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMB KU-A CH1 Targ Rng Est TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSMB KU-A Comm Radar RF Pwr TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Fuel Cell Auto Purge TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 1 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 2 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 3 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 1 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 2 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA FCP 3 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Suply H20 Dmp ISLN V TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Suply H20 Dmp Valve TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Waste H20 Dmp ISLN V TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Waste H20 Dmp Valve TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Flash Evap Cntrl Pri A-GPC CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Flash Evap Cntrl Pri B-GPC CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Flash Evap Cntrl Pri A CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA Flash Evap Cntrl Pri B CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA PL Pri Main B Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSA PL Pri Main C Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A RADAR Pass Mode TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A RADAR Out-Med TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A RADAR Out-Hi TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Comm A/RDR Mode TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Anten Strg Auto TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Anten Strg GPC DES TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Anten Strg GPC AGC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Rng Data TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB KU-A CH1 Rng Rate TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB GCIL KU-A Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB Rec Ops1 Tape Motion TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSB Rec Ops2 Tape Motion TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F1F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F1L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F1D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F2F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F2R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF1 Jet F2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F3F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F3L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F3U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F4R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F5L Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDF2 Jet F5R Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L1A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L1L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L2L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R1A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R1R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R2R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet R2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L5D Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA1 Jet L5L Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L3A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L3L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L4L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L4U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet L4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R3A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R3R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R4R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R4U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R5R Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSSC RJDA2 Jet R5D Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted GMT Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted GMT Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted GMT Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted GMT Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted GMT Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted MET Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted MET Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted MET Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted MET Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM Voted MET Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted GMT Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted GMT Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted GMT Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted GMT Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted GMT Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted MET Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted MET Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted MET Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted MET Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : CAS : CAS : CSTA MTU-PCM NonVoted MET Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:00:01 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCDV DV/Autochk TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCDV DV/Voltage TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCDV DV/Autochk Active TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCDV DV/Overflow TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCDV DVG Pressure TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA1 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA2 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA1 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA2 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA1 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA2 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA1 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA2 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA1 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGA EGA2 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGB EGA1 Offset I TSS:TSS-1:DCORE:DCORE:DCGB This virtual contains the DCORE EGA offset current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to millamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGB EGA2 Offset I TSS:TSS-1:DCORE:DCORE:DCGB This virtual contains the DCORE EGA offset current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to millamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGC EGA1 Acc Poten TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGC EGA2 Acc Poten TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGC EGA1 Fila V TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCGC EGA2 Fila V TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Analog Ref Mon1 TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Analog Ref Mon2 TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Masked Units Buf TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Health Status TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA TLC Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Configuration TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Remaining Seq TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Remaining Pul TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Rep Cmd Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMA Rep Mon Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Op Sys Warning B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Op Sys Warning B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Op Sys Warning B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CV Rpt Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CV Rpt Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CV Rpt Buf B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CV Rpt Buf B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CA Rpt Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB CA Rpt Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Masked Mon Buf B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Prgm Status B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Prgm Status B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Prgm Status B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Prgm Status B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Fault Mon Stat B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dump Add B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dump Add B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area2 B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area2 B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area3 B8 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area3 B9 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area4 B10 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area4 B11 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area5 B12 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area5 B13 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area6 B14 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB DCORE Dmp Area7 B15 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMB Mon Error Val TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA1 Fila I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA1 Fila I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA2 Fila I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA2 Fila I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA1 Tether I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA1 Tether I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA2 Tether I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMC EGA2 Tether I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Fmt Cntr TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Mem Addr TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Dmp Area2 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Dmp Area3 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Dmp Area4 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Dmp Area5 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCMD DCORE Dmp Area6 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 08:00:00 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm1 bits(0-31) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm1 bits(32-63) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm1 bits(64-95) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm2 bits(0-31) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm2 bits(32-63) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCME Apl Prgm2 bits(64-95) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA EGA1 Filament TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA EGA2 Filament TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA EGA1 High Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA EGA2 High Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA DV Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA CWGHS Swtch 1 TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA CWGHS Swtch 2 TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA CWGHS Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA DV Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA DV Hi Volt Swtch TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSA DV Autochk TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA1 Filament TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA1 HiPwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA1 Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA1 HiPwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA1 Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA2 Filament TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA2 HiPwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA2 Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA2 HiPwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EGA2 Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Swtch 1 TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Swtch 2 TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Swtch 1 Ver TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB CEGHS Swtch 2 Ver TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DV Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DV Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DV HV Swtch TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DV AutoChk TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DV Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DVG Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DVG Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DVG Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB PDECU Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB EOFF Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB QPM Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB PICV Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB STB Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB SIVC/LFCP Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB IDLE Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB DCORE ChkOut TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB Exe ChkOut TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB Trans Seq Go/Nogo TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCSB Trans In Prog TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA1 Fluid T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA2 Fluid T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA1 Head T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA2 Head T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA1 Fila PS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA2 Fila PS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA1 Coil T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA2 Coil T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA DVG T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA CEGHS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA DV T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA1 Xfomer T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA EGA2 Xfomer T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA PDECU T1 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA PDECU T2 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA PDECU T3 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA PDECU T4 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DCORE : DCORE : DCTA DVG DDCU T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-02 07:07:43 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHA SFMDM Cmd Cnt TSS:TSS-1:DPLY:DPLY:DPHA This virtual contains miscellaneous deployer housekeeping monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry for sensor 1 to integer The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHA Cmded Pwidth TSS:TSS-1:DPLY:DPLY:DPHA This virtual contains miscellaneous deployer housekeeping monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry for sensor 1 to integer The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd00 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd01 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd02 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd03 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd04 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd05 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd06 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd07 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd08 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd09 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd10 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd11 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd12 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd13 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd14 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd15 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd16 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd17 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd18 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd19 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd20 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd21 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd22 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd23 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd24 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd25 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd26 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd27 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd28 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHB SFMDM Cmd Wd29 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Offset TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Seg TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd00 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd01 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd02 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd03 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd04 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd05 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd06 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd07 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd08 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd09 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd10 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd11 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd12 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Rot Mem Dmp Wd13 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC ROM Chksum TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC Invalid Int Cnt TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHC RAM Chkout Fails TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHD Cur Seg Num In Prof TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHD % Time Ellapsed TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHD Time Remain TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHE Time Stmp TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHE Time Stmp Frm1 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPHE Time Stmp Frm2 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPMA CP Outbd Fine Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPMA CP Outbd Coar Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPMA CP Inbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 09:00:01 TSS : TSS-1 : DPLY : DPLY : DPMB Outbd Blended Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Cmded Outbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB 8Bit Inbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB % Basic Ctrl Mode TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Cmded Tether Acc TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Cmded Libra Vel TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Cmded Libra Ang TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Blended Ten Filt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Tether Len Filt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB REG V/Prop Ctrl TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMB Reg/Volt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMC Unstrtch Tether Len TSS:TSS-1:DPLY:DPLY:DPMC This virtual contains the measured tether length and rate. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters for sensor 0 and m/s for sensor 1 TABLE 1: polynomial coefficients taking telemetry to km for sensor 0 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 meters Sweep 0 1 0 km Sweep 1 0 0 meters/secs Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMC Tether Rate TSS:TSS-1:DPLY:DPLY:DPMC This virtual contains the measured tether length and rate. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters for sensor 0 and m/s for sensor 1 TABLE 1: polynomial coefficients taking telemetry to km for sensor 0 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 meters Sweep 0 1 0 km Sweep 1 0 0 meters/secs Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMD Tether Rate Raw Tmr Cnts TSS:TSS-1:DPLY:DPLY:DPMD This virtual contains the tether rate raw timer counts data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Ctrl Law Param 00 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Estimated Reel Rad TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Strtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded UnStrtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Spooled UnStrtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Spool Tether Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded In-Pl Libr Ang Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Est Reel Motor Ang Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Acc TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded In-Pl Libr Ang Acc TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Outbd Tension TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Outbd Blended Tension TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Elapsed Manu Time TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Motor/Gen Pulsewidth TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Load Res TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded Reel Motor Ter V TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Ctrl Law Param 12 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Ctrl Law Param 18 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cur Seg Dur Time TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cur Seg Init Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cur Seg End Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cur Seg Type TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPME Cmded In-Pl Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Latch Gr1 Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Latch Gr2 Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Boom Motors I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF MCA-Reel Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sat Bat Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sat P/L Mod Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sat Serv Mod Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF MPC-MCA I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF MPC Input I Hi Rng TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF MPC Input I Low Rng TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sat Ext Pwr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF MCP V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sat Ext Pwr V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Pri Upper Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Pri Lower Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Pri Boom Eject V1 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Pri Boom Eject V2 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Pri Boom Eject V3 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sec Upper Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sec Lower Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sec Boom Eject V1 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sec Boom Eject V2 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Sec Boom Eject V3 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Outbrd Fine Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Outbrd Coarse Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMF Inbrd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMG Mea Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMG Cmded Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMI Tether Len Raw Enc Cnts TSS:TSS-1:DPLY:DPLY:DPMI This virtual contains the tether length raw encoder counts data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMJ Meas DEL-L Cir1 TSS:TSS-1:DPLY:DPLY:DPMJ This virtual contains the tether DEL-L measurements. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters TABLE 1: polynomial coefficients taking telemetry to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 meters Sweep all 1 0 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMJ Meas DEL-L Cir2 TSS:TSS-1:DPLY:DPLY:DPMJ This virtual contains the tether DEL-L measurements. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters TABLE 1: polynomial coefficients taking telemetry to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 meters Sweep all 1 0 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPMK Reel Motor Cmd (Pwdth) TSS:TSS-1:DPLY:DPLY:DPMK This virtual contains the reel motor command (pulsewidth) There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA 0% Boom Retr 1 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA 0% Boom Retr 2 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA 100% Boom Exten 1 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA 100% Boom Exten 2 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Exten Mode TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Retr Mode TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Motor Sel TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Motor Dir Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Motor A ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Boom Motor B ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSA Enable InterBoom Stop Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC MCA Pwr TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC JTS Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC JTS Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC DPY/RTR Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC DPY/RTR Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Sat Int Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Sat Int Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Sgl Ended ADC V1 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Sgl Ended ADC V2 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Diff ADC V1 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSC Diff ADC V2 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 1 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 2 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 3 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 4 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 5 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch 6 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch Grp1 Open TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch Grp2 Open TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Open Latch Grp1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Open Latch Grp2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Close Latch Grp1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Close Latch Grp2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch Open Dir Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch Open Enable TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD Latch Open Dir TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSD At Least 4 Latches Clsd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Sep Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Spare1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Spare2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Retract 1 TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Full Retract 3 TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Sep TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U1 Sep Pwr TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U2 Sep Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U2 Sep TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSE U2 Sep Pwr TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Cir1 Sec TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Cir1 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Cir2 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Cir2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Disable1 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF L-DOT Disable2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF DEL-L Cir1 Sec TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF DEL-L Cir1 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF DEL-L Cir2 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF DEL-L Cir2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF Tklbk Status TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSF Tklbk Mon TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG MPC TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG MPC VCMD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG JTS Enable HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG JTS Enable D-Buf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG JTS Fire HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG JTS Fire D-Buf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG DPY/RTR Enable HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG DPY/RTR Enable DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG DPY/RTR Status HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG DPY/RTR Status DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Gyro Status DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG OBDH SlfChk DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG RAM Chkout TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG ROM Chkout TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Sat InLn Thrus DACA TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Sat InLn Thrus Nec TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Sat Hunt Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Sat TLM Buf Full TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Update Par Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Brake Sen Under V1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Brake Sen Under V2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Reel Lock Diseng2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Torq Test1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Torq Test2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Prop/Basic Ctrl Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG St Const PW Ret Enabled TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Ctrl Laws Active TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Inst Tether Dir1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Inst Tether Dir2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Motor/Gen Enable TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Resis Bank1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Resis Bank2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Reel Motor Enable TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Torq Test Cmd2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG APS Pres DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Bat Temp DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSG Gyro Temp DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH DACA Rdy For Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH DACA Cmd Auth TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH DACA Cmd Exe Suc TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH TLM Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH StaKping Man Hold TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH On Sta Status TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH TmOut Abort TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH Nom Cmd Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSH Motor/Gen Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSI SoftStop Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSI Resume To Sta1 Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSI Resume To Sta2 Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSI Resume To Dock Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSI SoftStop Man Exe TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Crit Func Relay Status TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Crit Func Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Ver Motor Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Ver Motor Clu Eng Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Ver Motor Rmpdwn Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ MCA Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ TT&C Pwr On Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Sat Bat Htrs Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Sat Ext Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Sat Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Dply Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Hot Nest Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ MPC ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ MPC VCMD Hi Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPSJ Crit Func Rly Cmp TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Mo Cld Plate T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Cvr T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Bearing Hs1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Bearing Hs2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Brake Motor T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Motor1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Reel Motor2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Boom Motor1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Boom Motor2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Boom Motor1 Ele T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTA Boom Motor1 Ele T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 1 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 2 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 3 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 4 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 5 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Latch 6 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Dock Ring Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Lnch Lock Diseng Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Load Bank 1 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Load Bank 2 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Load Bank 3 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Load Bank 4 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Struc Struts T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Struc Struts T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Sat Sup Struc T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Sat Sup Struc T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB DACA-PICA Cld Plate 5 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB MCA Cld Plate 6 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB MPC Cld Plate 10 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB LTCM Load Cell T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB LTCM Encoder T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Pallet T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Pallet T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB HVRA T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB HVRA T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB PICA 1 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB PICA 2 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB MCA T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB DACA T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB UTCM Struc T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Ver Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB Ver Motor Ele T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DPLY : DPLY : DPTB MPC T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : DRB : DRB : DBPO DRBA Header TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBPO DRBA Tip Pos TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBPO DRBD Header TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBPO DRBD Tip Pos TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBA Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBA Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBA P/L Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBA P/L Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBD Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBD Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBD P/L Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DRBD P/L Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA DPY/RTR Enable TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSA JTS Enable TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBA Stow SW Main:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBA Stow SW Main:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBA Stow SW Red:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBA Stow SW Red:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBD Stow SW Main:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBD Stow SW Main:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBD Stow SW Red:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DRBD Stow SW Red:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB Motor:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB Motor:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB CPU Watchdog:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB CPU Watchdog:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB DPT/RTR TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSB JTS Fire TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSC DPY/RTR Pwr TSS:TSS-1:DRB:DRB:DBSC This virtual consists of the power monitor flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBSC JTS Pwr TSS:TSS-1:DRB:DRB:DBSC This virtual consists of the power monitor flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBTA DRBA Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBTA DRBD Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : DRB : DRB : DBTA DRBE Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : EMP : EMP : EPMA EMP PCB T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP SFMDM Pri Core T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP SFMDM Sec Core T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Freon Pmp Out T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Freon Inlet T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Exp Freon Ret T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Pallet Struc T1 TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Pallet Struc T2 TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA DMS Temp TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Exp DC V TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Exp DC Cur TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Freon Pmp Inlet Pres TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Freon Pmp Dlta Pres TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMA EMP Freon Pmp Acc Quan TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 1 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 1 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 2 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 2 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 3 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 3 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 4 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 4 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 5 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 5 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 6 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 6 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 7 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 7 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 8 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 8 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 9 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 9 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 10 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 10 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 11 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 11 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 12 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 12 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 13 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 13 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 14 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 14 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 15 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 15 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 16 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB OCB 16 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB Type TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB Off In File TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 2 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 2 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 3 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 3 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 4 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 4 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 5 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 5 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 6 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 6 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 7 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 7 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 8 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMB VDB 8 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B1 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B2 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B3 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B4 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B5 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B6 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B7 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B8 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B9 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B10 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B11 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B12 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B13 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B14 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B15 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B16 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B17 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B18 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B19 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B20 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B21 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B22 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B23 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B24 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B25 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B26 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B27 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B28 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B29 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B30 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B31 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B32 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B33 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMC SFMDM Last Acc Cmd B34 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W1 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W2 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W3 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W4 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W5 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W6 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W7 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W8 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W9 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W10 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W11 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W12 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W13 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W14 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W15 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W16 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W17 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W18 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W19 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W20 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W21 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W22 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W23 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W24 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMD Limit CDTID (FSP) W25 TSS:TSS-1:EMP:EMP:EPMD This virtual contains the EMP CDTID (FSP) limit data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPME Limit Bits (FSP) W1 TSS:TSS-1:EMP:EMP:EPME This virtual contains the EMP limit bits (FSP) data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPME Limit Bits (FSP) W2 TSS:TSS-1:EMP:EMP:EPME This virtual contains the EMP limit bits (FSP) data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPME Limit Bits (FSP) W3 TSS:TSS-1:EMP:EMP:EPME This virtual contains the EMP limit bits (FSP) data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPME Limit Bits (FSP) W4 TSS:TSS-1:EMP:EMP:EPME This virtual contains the EMP limit bits (FSP) data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPME Limit Bits (FSP) W5 TSS:TSS-1:EMP:EMP:EPME This virtual contains the EMP limit bits (FSP) data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF No TECS in Buf TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF GMT-Nxt TEC to Exec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Lst Cmd Exec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Master Exec Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Sub Exec Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Entry # of Lst Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Eff GMT of Lst Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF DDCS MF Cntr TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C5 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C6 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C7 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Fname C8 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Exten C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Exten C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF TmLine Exten C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Master C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Master C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Master C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Master C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Master C5 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Sub C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Sub C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Sub C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Bkgnd Sub C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF DDCS GMT-Day TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF DDCS GMT-Sec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF DDCS RS422 Sync Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF No Of Invald Uplnk Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF DDCS Sys Perf TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMF Dsply No Sel TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Inpt Cmd Cntr TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Byte Cmd In Prog TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Core Swtch Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Sync Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Tele Fmt TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Fmt Id TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Cmd Rej Cnt TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Patch Cntr TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Pwr Fail TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM FVOS Err TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SFMDM Byte Err Code TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG EMP Byte Stat Reg TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG I/O Xfer TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG SDIO Acq Cmd FdBk TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Pri/Bkup Core Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG EMP Byte Cmd Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG EPROM Patch Test Sel TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG RAM Chksum TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMG Parser On Hold TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMH SFMDM RS-422 # of Bits TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMH SFMDM RS-422 Parity TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMH SFMDM RS-422 BaudRate TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMH SFMDM IO Xfer IOM Inpt Err TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPMH SFMDM IO Xfer # of Errs TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DMS Switch 1 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DMS Switch 2 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA EGA1 HP Enable TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA EGA2 HP Enable TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-EGA1 HP Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-EGA2 HP Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-EGA1 Coil Cur Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-EGA2 Coil Cur Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-DV +5V Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-DV Volt Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-DV Ovrflw Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pre-DVG Pres Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Dply Htr Pwr (K2) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DACA Pwr (K3) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Dply Pri Func Pwr (K4) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Sat Htrs/Cmd Pwr (K5) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Dply Sec Func Pwr (K6) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Sat Quies Htr Pwr (K7) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA EMP DC Pwr (K8) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA MPC Pwr (K9) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA EMP AC Pwr (K12) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pallet Cool Sys Pri Pwr (Pmp1) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Pallet Cool Sys Pri Pwr (Pmp2) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA MCP OCP Setpnt TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA SPREE Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DCORE Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA SETS Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA RTMD A TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA RTMD B TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA FDR 1 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA FDR 2 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA MCP A TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA MCP B TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Defl Plate A V TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA Defl Plate B V TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DDCU Tmline Mod TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSA DDCU GMT Mode TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg PS Byte Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg Int Bus TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg Data !Xfer TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg Ch !Pres TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg BSDIO Mod Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM EReg Pwr Int Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM GMT Invld TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM UART Frm Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM UART Ovrn Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM UART Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM UART Byte Mode Req TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS422 Stop Bit TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer Int Bus Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer Data !Xfer TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer Ch !Pres TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer !Suc TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM IO Xfer Re-EXEC Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR EPROM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR RAM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR ADC Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR CPU Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR APU Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR Mem Mod Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR Pwr Sup Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DCO Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR SDIO Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DO5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR RS422 SI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR PO5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DI5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR RIOUM1 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR RIOUM2 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DCIN Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR PO28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DO28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DI28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR GMTI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR DLM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR PRGI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM BSR PSPI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Mon Enab TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Ext Inpt TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Frm Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Ovrn Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Xfer Buf Emp TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM RS232 SW Data Rec TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Pri Core Act TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Bkup Core Act TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Othr Core Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Parbuf Unavail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Prsr Rej Cmd TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Sync Loss w/DDCU TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Invld Sync/Sour TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Invld IOM/CMD Id TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Invld Chksum TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSB SFMDM Maint Wd Cnt TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch00 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch01 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D05 Ch02 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch00 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch01 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSC SFMDM D28 Ch02 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch00 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch00 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch01 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch01 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch02 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch02 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch03 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSD SDIO Ch03 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit0 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit1 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit2 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit3 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit4 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit5 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit6 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : EMP : EMP : EPSE DDCS Fault Stat Bit7 TSS:TSS-1:EMP:EMP:EPSE This virtual contains the DDCS fault status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1992-08-02 04:45:39 1992-08-07 08:00:00 TSS : TSS-1 : RETE : RETE : RTAC AC-EF TSS:TSS-1:RETE:RETE:RTAC The RETE AC electric field measurements The following is a list of tables which are in this vidf TABLE 0: Lookup tables converting telemetry to volts for both high and low gain TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:57:46 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTBW Ex TSS:TSS-1:RETE:RETE:RTBW This virtual contains RETE burst mode AC wave acquisition data. The following is a list of tables which are in this vidf TABLE 0: lookup table decompressing telemetry giving N, a value proportional to power TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 microV**2 Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-04 08:59:47 1992-08-04 08:59:47 TSS : TSS-1 : RETE : RETE : RTBW Ey TSS:TSS-1:RETE:RETE:RTBW This virtual contains RETE burst mode AC wave acquisition data. The following is a list of tables which are in this vidf TABLE 0: lookup table decompressing telemetry giving N, a value proportional to power TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 microV**2 Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-04 08:59:47 1992-08-04 08:59:47 TSS : TSS-1 : RETE : RETE : RTBW Ez TSS:TSS-1:RETE:RETE:RTBW This virtual contains RETE burst mode AC wave acquisition data. The following is a list of tables which are in this vidf TABLE 0: lookup table decompressing telemetry giving N, a value proportional to power TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 microV**2 Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-04 08:59:47 1992-08-04 08:59:47 TSS : TSS-1 : RETE : RETE : RTBW Bx TSS:TSS-1:RETE:RETE:RTBW This virtual contains RETE burst mode AC wave acquisition data. The following is a list of tables which are in this vidf TABLE 0: lookup table decompressing telemetry giving N, a value proportional to power TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 microV**2 Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-04 08:59:47 1992-08-04 08:59:47 TSS : TSS-1 : RETE : RETE : RTBW Bz TSS:TSS-1:RETE:RETE:RTBW This virtual contains RETE burst mode AC wave acquisition data. The following is a list of tables which are in this vidf TABLE 0: lookup table decompressing telemetry giving N, a value proportional to power TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 microV**2 Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-04 08:59:47 1992-08-04 08:59:47 TSS : TSS-1 : RETE : RETE : RTCA WRA: Band A TSS:TSS-1:RETE:RETE:RTCA This virtual contains the RETE AC electromagnetic data in the calibration cycle for band A in the low frequency range. The calibration cycle has eight steps of unequal duration. Step 1 : Gen clock : SLOW. Gen level : HIGH=7. Phase : 0. B cal : OFF. Attn : OFF. Calibration of RTLA is performed simultaneously with four calibrations of RTMC then four calibrations of RTMD. Step 2 : Gen clock : SLOW. Gen level : 0 -> 7. Phase : 0. B cal : OFF. Attn : OFF. Amplitude calibration is performed simultaneously on RTLB and RTMC; on each, eight levels are sampled sequentially, with the attenuators off. Step 3 : Gen clock : FAST. Gen level : 0 -> 7. Phase : 0. B cal : OFF. Attn : OFF. Amplitude calibration is performed on RTME and RTMF, and simultaneously of RTHF. In the MF calibration at each of the 8 amplitude levels there are 2 calibrations of RTME followed by 4 calibrations of RTMF. In the HF calibration, on each amplitude level there are 8 frequencies calibrated in steps of 32, the 1st frequency being chosen between 0, 1, 2 and 3. On steps 4, 5, 6 and 7, the phase determination is calibrated. On each step, there is one calibration of RTMD, RTME and RTMF. Step 4 : Gen clock : FAST. Gen level : HIGH=7. Phase : 0. B cal : OFF. Attn : ON. Step 5 : Gen clock : SLOW. Gen level : HIGH=7. Phase : -45, 45. B cal : OFF. Attn : ON. Step 6 : Gen clock : SLOW. Gen level : HIGH=7. Phase : -45, 45. B cal : OFF. Attn : ON. Step 7 : Gen clock : FAST. Gen level : 3 ?. Phase : 0. B cal : OFF. Attn : OFF. Step 8 : Gen clock : OFF. Gen level : OFF. Phase : n/a. B cal : ON. Attn : ON. The magnetic search coils are calibrated. The calibration signal is injected onto a test winding on each of the three coils. Simultaneously, a single calibration of RTLB, consecutive calibrations of RTMC, RTMD, RTME and RTMF, and 8 channels of RTHF are calibrated eight times. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 11:06:55 TSS : TSS-1 : RETE : RETE : RTDP V1 TSS:TSS-1:RETE:RETE:RTDP The RETE double probe data The following is a list of tables which are in this vidf TABLE 0: Lookup table converting telemetry to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor all 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 05:33:49 1992-08-04 11:25:19 TSS : TSS-1 : RETE : RETE : RTDP V2 TSS:TSS-1:RETE:RETE:RTDP The RETE double probe data The following is a list of tables which are in this vidf TABLE 0: Lookup table converting telemetry to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor all 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 05:33:49 1992-08-04 11:25:19 TSS : TSS-1 : RETE : RETE : RTEF DC-EF: (V1-V2) TSS:TSS-1:RETE:RETE:RTEF The RETE Langmuir probe DC, 0-2 Hz, electric field measurements. For these measurements the two dipole probes are run either in the biased or unbiased state (at one of 3 different current values). The states are selected by telecommand. In addition the probes can be set by telecommand to be in a high or low gain state. The default state is no bias, low gain. The sampling rate depends on the instrument mode (5/sec in NM, and 32/sec in PP2). The following is a list of tables which are in this vidf TABLE 0: Lookup tables converting telemetry to volts for both high and low gain TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTHF Ex TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTHF Ey TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTHF Ez TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTHF Bx TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTIP Ion Probe I TSS:TSS-1:RETE:RETE:RTIP The RETE ion probe current. The sensor is a simple electrostatic ion trap (Faraday Cup), biased at a fixed voltage of -7.5V with respect to the canaster. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting telemetry to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Overrun Cntr TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Watchdog Cntr TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB DCE Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB DCPB Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB V1 TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB V2 TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB +50V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB +25V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB +12V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB +5V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB -5V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB -12V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB -25V Sup Line TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB +5V Ref TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB -5V Ref TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Pentode Plate V TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Pentode I Setting TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Pentode Res Setting TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Pentode Cathode I TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Pentode Grid V TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Ext Plasma Pkg Mode TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Int Plasma Pkg Mode TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKB Frame Cntr TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE DC housekeeping monitors. Note that the scaling table for the Pentode Resister Mode data (sensors 15-19) was generated with a 200 V power supply between the spacecraft ground and the DCBP The telemetry from sensors 6-15, 18-19 are converted to physical units according to the formula: V = S * [B*exp{T * log(256)/A} + C] + Z where: V is the converted value S is the sign (calibration set 1) A is either 128 or 127 (calibration set 0) B,C polymonials coefficients converting modified telemetry to physical units (table 2) Z is an offset value (table 4) The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 2-3 to degrees C, from sensors 4-5 to volts and from sensors 16-17 to microamps TABLE 1: lookup table converting telemetry from cal set 0 to ln(256)/128 or ln(256)/127 TABLE 2: polynomial coefficients converting processed data output from TABLE 1 to volts for sensors 6-14 and 19, to kilovolts for sensor 15 and mucroamps for sensor 18 TABLE 3: lookup table converting cal set 1 to sign TABLE 4: offsets for sensors 6-15, offsets for sensors 18-19 are 0 and not included The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1,20-22 - - integer Sweep 2-3 0 0 degrees C Sweep 4-5 0 0 volts Sweep 16-17 0 0 microamps Sweep 6-14 1,2,3,4 13,0,3,1 volts Sweep 15 1,2,3,4 13,0,3,1 kilovolts Sweep 18 1,2,3 13,0,3, microamps Sweep 19 1,2,3 13,0,3, volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:49 TSS : TSS-1 : RETE : RETE : RTKC Ram Add Line TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Checksum TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Exceeding Data TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Overrun TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Framing TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Parity TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC HF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC MF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC LF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKC Exceeding Samp TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKD TeleCmd Echo TSS:TSS-1:RETE:RETE:RTKD This virtual contains the RETE telecommand echo. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKE Pentode/I TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKE DCBP/Pot TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKF RETE Mode TSS:TSS-1:RETE:RETE:RTKF This virtual contains the RETE format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKF RETE Pg# TSS:TSS-1:RETE:RETE:RTKF This virtual contains the RETE format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKG LF Mode TSS:TSS-1:RETE:RETE:RTKG This virtual contains the RETE LF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKG LF Sens TSS:TSS-1:RETE:RETE:RTKG This virtual contains the RETE LF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTKH MF Input 1 Sens TSS:TSS-1:RETE:RETE:RTKH This virtual contains the RETE MF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the sensor telemetry There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 11:06:55 TSS : TSS-1 : RETE : RETE : RTKH MF Input 2 Sens TSS:TSS-1:RETE:RETE:RTKH This virtual contains the RETE MF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the sensor telemetry There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 11:06:55 TSS : TSS-1 : RETE : RETE : RTKI HF Mode TSS:TSS-1:RETE:RETE:RTKI This virtual contains the RETE HF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 11:06:55 TSS : TSS-1 : RETE : RETE : RTKI HF Sens TSS:TSS-1:RETE:RETE:RTKI This virtual contains the RETE HF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1992-08-03 04:41:22 1992-08-05 11:06:55 TSS : TSS-1 : RETE : RETE : RTLA Ex TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTLA Ey TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTLA Ez TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTLA Bx TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTLA Bz TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1992-08-03 03:38:18 1992-08-05 10:59:16 TSS : TSS-1 : RETE : RETE : RTLB Ex TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1992-08-03 03:38:27 1992-08-05 10:59:25 TSS : TSS-1 : RETE : RETE : RTLB Ey TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1992-08-03 03:38:27 1992-08-05 10:59:25 TSS : TSS-1 : RETE : RETE : RTLB Ez TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1992-08-03 03:38:27 1992-08-05 10:59:25 TSS : TSS-1 : RETE : RETE : RTLB Bx TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1992-08-03 03:38:27 1992-08-05 10:59:25 TSS : TSS-1 : RETE : RETE : RTLB Bz TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1992-08-03 03:38:27 1992-08-05 10:59:25 TSS : TSS-1 : RETE : RETE : RTLP Curent TSS:TSS-1:RETE:RETE:RTLP This IDFS contains the RETE Langmuir Probe data. There were several problems found with this portion of the experiment which effected the data. It is suggested that the experimenters be contacted before use of this data set. Corrections are available directly through the PI group. The following is a list of tables which are in this vidf TABLE 0: Base scan table TABLE 1: Cal Set 0 to scan length TABLE 2: Cal Set 1 to scan decrement value (volts) TABLE 3: Cal Set 2 to scan beginning volatage value (volts) TABLE 4: Conversion of telemetry to amps TABLE 5: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0,1,2,3 0,4,3,1 volts Sweep 4 0 amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 35 1992-08-03 04:41:22 1992-08-05 11:07:01 TSS : TSS-1 : RETE : RETE : RTMC Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMC Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:55 1992-08-05 11:07:27 TSS : TSS-1 : RETE : RETE : RTMD Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTMD Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:57 1992-08-05 11:07:29 TSS : TSS-1 : RETE : RETE : RTME Ex: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Ey: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Ez: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Bx: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Bz: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Ex: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Ey: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Ez: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Bx: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Bz: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTME Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : RETE : RETE : RTMF Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1992-08-03 04:41:58 1992-08-05 11:07:30 TSS : TSS-1 : ROPE : ROPE : RPBB BMSP I TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and voltage responding to the differential charge between the ROPE instrument boom and the satellite The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPBB BMSP V TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and voltage responding to the differential charge between the ROPE instrument boom and the satellite The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Num of Peaks TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 1: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 2: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 3: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 1: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 2: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDM Peak 3: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDP Defl TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDP Retard TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDP Retard/Pk 1 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDP Retard/Pk 2 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPDP Retard/Pk 3 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPEA e- Sen 3 TSS:TSS-1:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:35 TSS : TSS-1 : ROPE : ROPE : RPEA e- Sen 4 TSS:TSS-1:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:35 TSS : TSS-1 : ROPE : ROPE : RPEA e- Sen 5 TSS:TSS-1:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:35 TSS : TSS-1 : ROPE : ROPE : RPEB e- Sen 1 TSS:TSS-1:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:30 TSS : TSS-1 : ROPE : ROPE : RPEB e- Sen 2 TSS:TSS-1:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:30 TSS : TSS-1 : ROPE : ROPE : RPEM Dif/Elec TSS : TSS-1 : ROPE : ROPE : RPEM This virtual instrument contains the DIFP electrometer data The following is a list of tables which are in this vidf TABLE 0: lookup table converting telemetry to amps The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 4 1992-08-03 04:51:30 1992-08-05 11:23:39 TSS : TSS-1 : ROPE : ROPE : RPHA FmtCntr/Lo TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA FmtCntr/Hi TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA Cyc/Cntr TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA Cmd/Word TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA DIFP-E/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA DIFP-S/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHA EPROM/Chksm TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB DifV -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB RtdV 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHB ColI 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 1 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 1 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 2 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 2 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 30V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC HVPS 30V I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC PPS1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHC PPS2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES1/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES2/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES3/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES4/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES5/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES1/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES2/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES3/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES4/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHD SPES5/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP 0V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FS +28V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FS +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FS +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FS -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FS 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE FPS T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE HVPS1 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE HVPS2 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE CEP El T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHE MF Cntr TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPHF PPS1/+V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-04 08:22:06 1992-08-05 02:04:06 TSS : TSS-1 : ROPE : ROPE : RPHF PPS1/-V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-04 08:22:06 1992-08-05 02:04:06 TSS : TSS-1 : ROPE : ROPE : RPHF PPS2/+V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-04 08:22:06 1992-08-05 02:04:06 TSS : TSS-1 : ROPE : ROPE : RPHF PPS2/-V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1992-08-04 08:22:06 1992-08-05 02:04:06 TSS : TSS-1 : ROPE : ROPE : RPHG FPS I/Monitor TSS | TSS-1 | ROPE | ROPE | RPHG This virtual instrument contains the floating power supply (FPS) current monitor. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to uamps The following are units which can be derived from the tables. TYPE TABLES OPERS UNIT swp 0 0 microamps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPIA p+ Sen 3 TSS:TSS-1:ROPE:ROPE:RPIA This virtual consists of data from the satellite mounted ion SPES sensor. The sensors is mounted at an azimuthal angle of 135 degrees from the science boom and at a polar angles of 0 degrees. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Ion Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:35 TSS : TSS-1 : ROPE : ROPE : RPIB p- Sen 1 TSS:TSS-1:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:30 TSS : TSS-1 : ROPE : ROPE : RPIB p- Sen 2 TSS:TSS-1:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1992-08-03 04:01:52 1992-08-05 02:03:30 TSS : TSS-1 : ROPE : ROPE : RPSA SPES 1 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA SPES 2 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA SPES 3 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA SPES 4 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA SPES 5 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA HVPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA HVPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA PPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSA PPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB FPS Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB FPS Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB FPS Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS1 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS1 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS1 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS2 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS2 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB PPS2 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB HVU Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB Grid Bias Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB Macro Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB DIFP Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB FPS Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB Tele Test TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSB End Cmd TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Pot:Seek Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Pot:Track Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Pot:Seek/Track Fail TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Pwr Comsump. TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Perf Pwr Consump Chk TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Bad Readings TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Bad FPS/V Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSC Bad BMSP/I Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD RAM/Tmr1/T1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD RAM/Tmr1/T2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD RAM/Tmr2/T1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD RAM/Tmr2/T2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD 2K/RAM/T1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD 2K/RAM/T2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD 8K/RAM/T1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : ROPE : ROPE : RPSD 8K/RAM/T2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SAHK : SAHK : SHAA Yaw Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAA Roll Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAA Roll Update Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAA Pitch Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAA Pitch Update Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Yaw Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Yaw Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Roll Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Roll Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Pitch Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAB Scaled Pitch Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC X Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC Y Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC Z Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC S Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC ES1 Sun Pres TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAC ES2 Sun Pres TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAD Alpha Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAD Beta Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAD Gamma Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAD Skew Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Coarse Const X Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Coarse Const Y Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Coarse Const Z Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Coarse Const S Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Fine Const X Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Fine Const Y Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Fine Const Z Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Fine Const S Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Ref Hold Ang TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Const Ref Hold Ang TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAE Yaw Rate TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAF Ref Spin Rate TSS:TSS-1:SAHK:SAHK:SHAF This virtual contains the satellite spin rate data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to radians/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAF Cur Ref Spin Rate TSS:TSS-1:SAHK:SAHK:SHAF This virtual contains the satellite spin rate data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to radians/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG Alpha 1/2 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG Alpha 3/4 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG Beta 1/2 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG Beta 3/4 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG ES1 Chord 1 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG ES1 Chord 2 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG ES2 Chord 1 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHAG ES2 Chord 2 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA Flag 3 (Test) TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA TLC Buf 1 Error TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA TLC Buf 2 Error TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA Warmup TmOut TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA TULC TmOut TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA AMSAS Entry Pnt TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA TULC 1st NOGO TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA Scaled Tm To Dock TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA I/O Pl Oper Mode TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA SAS 1st Run TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA SAS InLn2 Closed Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA SAS InLn2 Open Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHA TUCL InLn2 Closed Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHB Onboard Time TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHB Bat1/Bat2 Int Cur TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHB Bat3/Bat4 Int Cur TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHB Sat Ener Consump TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHB P/L Ener Consump TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Elapsed Time TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Crew Sleeping Time TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Long TULC Timeout TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Time To Docking TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Time To Dplyment TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHC Time To Retrieval TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD Cmd Mode TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD 1st Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD 2nd Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD 3rd Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD Updating Proced Run TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD Nshot TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHD Fire Pos/Neg TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHE I/O Pl Sel Valve TSS:TSS-1:SAHK:SAHK:SHHE This virtual contains the low time resolution satellite 3 bit monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor 1 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHE Phase Id # TSS:TSS-1:SAHK:SAHK:SHHE This virtual contains the low time resolution satellite 3 bit monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor 1 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHF RX Coherent AGC TSS:TSS-1:SAHK:SAHK:SHHF This virtual contains the satellite RX Coherent AGC and loop stress monitors The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry for sensor 0 t0 DbM telemetry for sensor 1 to degrees The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 DbM Sweep all 0 0 degrees G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHHF Loop Stress TSS:TSS-1:SAHK:SAHK:SHHF This virtual contains the satellite RX Coherent AGC and loop stress monitors The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry for sensor 0 t0 DbM telemetry for sensor 1 to degrees The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 DbM Sweep all 0 0 degrees G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:1 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:2 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:3 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:4 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:5 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:6 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:7 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMA OBDH RSMN:8 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMB OBDH ASMIN CH T1 TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMB OBDH ASMIN CH T2 TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMB OBDH ASMIN CH T1 RTUP TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMB OBDH ASMIN CH T2 RTUP TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp St Add TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D1 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D1 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D1 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D1 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D2 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D2 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D2 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D2 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC DH UP MDmp D3 TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp St Add TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC AMCS UP MDmp D3 TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Cntr TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf1 Msg# TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf2 Msg# TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf1 Exp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf2 Exp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf1 Comp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC TLC Buf2 Comp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC Fmt Cntr TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMC Fmt Num TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH PROM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH G-RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH FGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH BGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH Subr Err TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH Stck Ovrflow TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD OBDH Self Chk TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS Up Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS PROM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS G-RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS FGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS BGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS Subr Err TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS Stck Ovrflow TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS Self Chk TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD AMCS GR Acc Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD BUS Arbtr Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD RTUS Arbtr Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD GR Access Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD > 2 Blks TLCS TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD CTU-RTUS Link TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHMD CTU-RTUP Link TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHME OBDH FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHME OBDH BGF # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHME AMCS FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHME AMCS FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHME AMCS Oper. Mode TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat1/Bat2 I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat4/Bat4 I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Main Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA OBDH Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA TT&C Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA PPDA Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA AMCS Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA PM Heater Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA D&J Heater Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA I/O Pl Sec Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA APS Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Yaw Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Rel/L Valve Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat 2 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat 4 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat1/Bat2 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Bat3/Bat4 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA Main Bus V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA TX Reg V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA RX Reg V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHPA TX RF Output Pwr TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Status TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA X Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Y Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Z Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA S Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA X Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Y Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Z Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA S Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Pkg 1 X Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Pkg 1 Z Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Pkg 2 Y Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Gyro Pkg 2 S Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA X Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Y Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Z Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA S Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Earth Sen TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Sun Sen TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA EL/1 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA EL/2 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/1 Served TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/2 Served TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/1 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/2 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/1 Hd Flg TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/2 Hd Flg TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/1 Int Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA ES/2 Int Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Yaw 1 Cmd Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Yaw 2 Cmd Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Yaw 1 Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSA Yaw 2 Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB X Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Y Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Z Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB S Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB X Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Y Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Z Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB S Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB X Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Y Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB Z Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSB S Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSC FDS3/FDS4 Status TSS:TSS-1:SAHK:SAHK:SHSC This virtual contains the low time resloution satellite FDS3/FDS4 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSC FDS3/FDS4 Sun TSS:TSS-1:SAHK:SAHK:SHSC This virtual contains the low time resloution satellite FDS3/FDS4 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD GYMODE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD GYOPS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD GYCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD GYWU Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD GYRO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ACQGYR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ATTITUDE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PASSIVE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SPIN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD HOLD Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD RETR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ONST Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD DEPL Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD VRPH1 Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD VRPH2 Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD RTUPQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD RTUSQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD TIMSLEEP Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD TIMCOUNT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD Start Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD IOFIRE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD CA Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD TFGEN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ICOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD LM Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SRM Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD RERE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ROMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PRPO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD TTOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SAS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD TULC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PMTC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PEPC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD PEPC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD DPPH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SWITCH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD AQTEST Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD CONTROL Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD AFTGEN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ACA Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD AICOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SVISOR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD AMSAS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD UPDAT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD AROMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD YAWTH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD APCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ESCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD SSTC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSD ESUP Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 01: ROPE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 09: ROPE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 02: ROPE Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 03: TEMAG Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 04: TEMAG Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 07: RETE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 08: RETE Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 06: Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE P/L 12: Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE GPS Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE Main Iso Valve TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE In Line 1 Valve TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE RX Lock TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE Temp 3 Warning TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSE Temp 4 Warning TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Bat1/Bat2 Cur Sign TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Bat3/Bat4 Cur Sign TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Temp1 Warning TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Temp2 Warning TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF InPl Rear Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF InPl Front Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF OutPl Right Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF OutPl Left Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF ES1 Pwr TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF ES1 Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF ES2 Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Ranging Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Squelch Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF Frame Valid TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSF ASW Found TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Test Bit Sign TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG P/L Energy Consump TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Uplink Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Valve1 NOGO TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Valve2 NOGO TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Pwr Off Cmd Sent TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Pwr Drop Occur TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG APS Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Crit Fn Rly Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg1 Squelch TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg1 RX Coher AGC TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg1 Lock Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Updating Enabled TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG APS Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Reg Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Tank Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg5 PM Sec1/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg5 PM Sec2/T2 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg5 PM Sec3/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg6 PM Sec1/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg6 PM Sec2/T2 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Flg6 PM Sec3/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat1 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat2 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat3 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat4 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG APS Pres Reg Temp TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSG Bat Verification TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH InLine 2 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH I/O OfPl Iso Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH Yaw 1 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH Yaw 2 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH ES1 Pwr TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSH TX Pwr TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI Bat1/Bat2 Status TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI Bat3/Bat4 Status TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI TT&C Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI PPDA Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI AMCS Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI APS Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI PM Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI I/O Pl Sec Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI Yaw Sec Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSI TX Pwr Enable TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Alpha 1/2 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Alpha 3/4 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Beta 1/2 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Beta 3/4 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Alpha 1/2 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Alpha 3/4 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Beta 1/2 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ Beta 3/4 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ FDS1/FDS2 Status TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSJ FDS1/FDS2 Sun TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK Yaw/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK Yaw/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK InPl/Rear TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK InPl/Frnt TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK OutPl/Right TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK OutPl/Left TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK InLn/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHSK InLn/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA Gyro Pkg 1 Temp X TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA Gyro Pkg 1 Temp Z TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA Gyro Pkg 2 Temp Y TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA Gyro Pkg 1 Temp S TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA ES1 Int Temp TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTA ES2 Int Temp TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec1 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec1 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec2 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec2 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec3 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec3 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec4 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Sec4 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec1 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec1 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec2 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec2 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec3 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec3 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec4 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB PM Skin Sec4 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T3 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T4 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T5 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T6 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T7 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T8 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T9 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T10 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T11 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T12 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T13 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T14 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T15 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Env T16 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T3 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T4 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T5 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T6 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T7 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTB SM Skin T8 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Tank Pres TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Regulated Pres TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Battery 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Battery 2 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Battery 3 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC Battery 4 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS Pres Reg Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS Tank Sur Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS Out Tank Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS ATH 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS ATH 3 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS InLine 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS InLine 2 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS InPl Rear Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS InPl Frnt Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS OutPl Valve Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS I/OutPl Iso Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC APS Yaw 1/2 Valve Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC TX Final Stge Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SAHK : SAHK : SHTC RX Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1992-08-03 03:38:51 1992-08-04 05:59:50 TSS : TSS-1 : SCORE : SCORE : SCAC SLA/X TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCAC SLA/Y TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCAC SLA/Z TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCAF SLA/X TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCAF SLA/Y TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCAF SLA/Z TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMA SLA:Coarse T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMA SLA:Fine T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMA SLA:Filter T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMA SLA:DC/DC Reg V TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMB SA:Temp TSS:TSS-1:SCORE:SCORE:SCMB This virtual contains the SA temperature and overtemperature housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensor 0 to degrees C and sensor 1 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 degrees C Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMB SA:OverTemp TSS:TSS-1:SCORE:SCORE:SCMB This virtual contains the SA temperature and overtemperature housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensor 0 to degrees C and sensor 1 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 degrees C Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMC SV/Ovflow TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMC SV/Achk/S TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMC SV/AChk TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCMC Tether/I TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSA P/L Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSA H/K Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSA P/L 05 SA Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSA P/L 10 SLA Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSA P/L 11 HTR Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSB SLA Oper TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSB SA Pwr Chk TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SCORE : SCORE : SCSB SA Autochk Cmd TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1992-08-03 03:38:51 1992-08-05 10:59:49 TSS : TSS-1 : SETS : SETS : STAA Bx TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STAA By TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STAA Bz TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCA Cur Den (Peak) TSS:TSS-1:SETS:SETS:STCA This virtual contains the peak monitors in the SETS current and charge probe The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCA Charge Den (Peak) TSS:TSS-1:SETS:SETS:STCA This virtual contains the peak monitors in the SETS current and charge probe The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCB Cur Den (Dir) TSS:TSS-1:SETS:SETS:STCB This virtual contains the SETS direct current and charge probe monitors. The data is transmitted as separate 8 and 4 bit values and is combined within this virtual to a single 12 bit data word. The 4 bits is the lowest 4 bits. The telemetry scaling to physical units was given only for the 8 bit data, of the form Value = A + Tele * B To compensate for adding the bottom 4 bits, the scaling factor B has been divided by 16 in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCB Charge Den (Dir) TSS:TSS-1:SETS:SETS:STCB This virtual contains the SETS direct current and charge probe monitors. The data is transmitted as separate 8 and 4 bit values and is combined within this virtual to a single 12 bit data word. The 4 bits is the lowest 4 bits. The telemetry scaling to physical units was given only for the 8 bit data, of the form Value = A + Tele * B To compensate for adding the bottom 4 bits, the scaling factor B has been divided by 16 in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Cur Filter In TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Cur Calib TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Cur Enable TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Q Reset TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Q Enable TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Relay TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCC CCP Pwr TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP Probe Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP +15V Bus V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP -15V Bus V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD Q Probe Off V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD Cur Probe Off V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD CCP Current TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STCD Time CCP Rlys On TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA DEP MN Frm Cur Cnt TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA Fault Code1 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA Fault Code2 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA FLT1 Running Tot TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA FLT2 Running Tot TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA Oper Mode TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA Oper Cycle TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA Oper Step TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA DEP Msg Stat Wd TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA DEP I TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA DEP T1 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDA DEP T2 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDB OCI Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDB OMI Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDB Step Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDB CPU Tm at Mn Frm 0 Req TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDB TM Pg Chksum TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDC CPU On Time TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDC Multibus Tm Bytes 1-3 TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDC Multibus Tm Bytes 4-6 TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDC Mn Frm Cnt 0 Time TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STDC GMT TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG Current TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 Focus Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 Anode Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 HV Conv Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 Focus Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 Anode Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 HV Conv Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 Charge Out TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 Charge Out TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 Pre-reg +20V TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 HVPS TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 Pre-reg +20V TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 HVPS TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun1 Fila Conv T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun2 Fila Conv T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Gun Elec T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG +15V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG +5V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG -15V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG # Pulses TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG Pulse Off Tm TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG Pulse On Tm TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA Time FPEG Fila On TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFA FPEG Cmd Cntr TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Pwr TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB EGA Sync1 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB EGA Sync2 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Enable Pulses Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Enable Off Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Enable On Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Fila Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Fila Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Fila On Tmr Set TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Fila On Disc TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG HV Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG HV Enable Var TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG HV Arm TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG HV On TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Run Bar Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Gun1 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Gun2 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Run TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Stop TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Stret Gun Pulse TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Go Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Send Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Ready Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Cur Limit TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB FPEG Squel Enable TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STFB Gun Sw Pulse Mon TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMA Heater Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMA SRPA Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMA SPIB Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMA AMAG Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB AMAG Current TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB SPIB Current TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB SPIB Voltage TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB SPIB T1 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB SPIB T2 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STMB SPIB T3 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSA LangP Swping TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSA LangP Flybk TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSA LangP Srch Mode TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSA LangP Short Swp TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Hi Sens SRPA Swping TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Hi Sens SRPA Flybk TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Hi Sens SRPA Srch Mode TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Hi Sens SRPA Short Swp TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Low Sens SRPA Swping TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Low Sens SRPA Flybk TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Low Sens SRPA Srch Mode TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSB Low Sens SRPA Short Swp TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC Htr Cur TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC SRPA Cur TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC +6V SRPA Bus V TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC -6V SRPA Bus V TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC 10.5 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC 8.5 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC LP 3.2 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC Analyzer Elec T TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STSC Preamp T TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTA Tether I TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS tether current monitor. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps TABLE 1: polynomial coefficients taking telemetry to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 0 1 0 milliamps Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Current TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM +15V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM +5V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM -15V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM +28V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Base Plate T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Pwr Sply T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Load RisA T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Load RisB T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Load RisC T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM PROT Cap T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Elec T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Pres A TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Pres B TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM Lst Cmd Sent TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTC TCVM TVM AC Gain Rlys TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Pwr TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/CAL A/C TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TVM/AC/FC TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TCM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TCM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM TCM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Mux Add B0 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Mux Add B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Mux Add B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Mux Add B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Hskp Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/Gain/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/Gain/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/LPFR/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/LPFR/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/LPFR/ B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMS/Relay TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMS/DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM CMS/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Shunt Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Shunt DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Shunt Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM 2.5 Mohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM 250 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM 25 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM HV Prot TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD TCVM Mech Mode Sw TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SETS : SETS : STTD Prot Cap En Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1992-08-02 04:59:23 1992-08-07 09:00:01 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod EL7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Ch7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPBA Space Beam Mod Sig7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z0 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z1 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z2 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z3 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z4 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z5 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z6 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z7 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z8 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEA Electrons/A Z9 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z0 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z1 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z2 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z3 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z4 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z5 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z6 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z7 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z8 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEB Electrons/B Z9 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z0 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z1 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z2 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z3 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z4 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z5 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z6 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z7 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z8 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPEC Electrons/A Z9 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z0 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z1 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z2 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z3 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z4 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z5 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z6 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z7 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z8 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPED Electrons/B Z9 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:46 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFA e- Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPFB e- Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:54 1992-08-06 01:00:01 TSS : TSS-1 : SPREE : SPREE : SPHA DPU Base Plate T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA DPU Pwr Supply T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA DPU FDR1 Casing T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA DPU FDR2 Casing T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA HV A Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA HV B Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA MCP A Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA MCP B Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA RTMD A Motor T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA RTMD B Motor T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA MCP A V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA MCP B V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA +5V Line V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA +12V Line V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA Dif Plate A V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHA Dif Plate B V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR1 Tape Xsport T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR1 Casing T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR1 Pressure TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR1 Rd/Wr Err Cnt TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR2 Tape Xsport T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR2 Casing T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR2 Pressure TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHB FDR2 Rd/Wr Err Cnt TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHC FDR1 Tape Cntr TSS:TSS-1:SPREE:SPREE:SPHC This virtual contains the SPREE tape counter monitors. There are no tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHC FDR2 Tape Cntr TSS:TSS-1:SPREE:SPREE:SPHC This virtual contains the SPREE tape counter monitors. There are no tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHD Space Frm Cnt TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHD Space Frm Size TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHD Space Rot Num TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHD Energy Swp Num TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPHE Uplink Cmd Echo TSS:TSS-1:SPREE:SPREE:SPHE This virtual contains the SPREE uplink command echo. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIA SumIons/A TSS:TSS-1:SPREE:SPREE:SPIA This virtual contains the SPREE summed ion spectrum from ESA A. This particular summed spectrum contains the particle counts divided by 8 to avoid overflow and then summed over all 10 elevation angles (SPREE zones 0-9). Summation of the zones occurs before the division by eight. The division is done regardless of the energy sweep rate. This summed spectrum then contains the particle count at each of the 32 energy levels, summed over zone. If the instrument is in the 8 energy sweeps/sec mode, the summed spectra provided in this telemetry block will be from the energy sweep matching the highest potential determination. If the potential value is 0 or exactly the same for all 8 energy sweeps, the downlinked summed spectrum in the first of the 8. If in the 1 energy sweep/sec mode, these data correspond to the potential information by default. This portion of the telemetry is intended to provide the closest correspondence to the potential determination, specifically for crew use on the PGSE display. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIB SumIons/B TSS:TSS-1:SPREE:SPREE:SPIB This virtual contains the SPREE summed ion spectrum from ESA B. This particular summed spectrum contains the particle counts divided by 8 to avoid overflow and then summed over all 10 elevation angles (SPREE zones 0-9). Summation of the zones occurs before the division by eight. The division is done regardless of the energy sweep rate. This summed spectrum then contains the particle count at each of the 32 energy levels, summed over zone. If the instrument is in the 8 energy sweeps/sec mode, the summed spectra provided in this telemetry block will be from the energy sweep matching the highest potential determination. If the potential value is 0 or exactly the same for all 8 energy sweeps, the downlinked summed spectrum in the first of the 8. If in the 1 energy sweep/sec mode, these data correspond to the potential information by default. This portion of the telemetry is intended to provide the closest correspondence to the potential determination, specifically for crew use on the PGSE display. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z0 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z1 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z2 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z3 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z4 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z5 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z6 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z7 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z8 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIC Ions/A Z9 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z0 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z1 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z2 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z3 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z4 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z5 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z6 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z7 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z8 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPID Ions/B Z9 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z0 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z1 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z2 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z3 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z4 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z5 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z6 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z7 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z8 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIE Ions/A Z9 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z0 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z1 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z2 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z3 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z4 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z5 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z6 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z7 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z8 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPIF Ions/B Z9 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLA p+ Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLB e- Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:48 1992-08-07 12:00:01 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLC p+ Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:50 1992-08-07 12:00:02 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPLD e- Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1992-08-02 07:37:52 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPMF Bx TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPMF By TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPMF Bz TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Orb Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Conf Fac TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Head Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Zone Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Ch Above Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Peak Channel TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPOP Ch Below Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 0 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 1 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 2 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 3 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 4 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 5 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 6 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 7 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 8 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 9 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 10 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Low Freq MMU 11 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b0 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b1 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b2 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b3 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b4 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b5 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b6 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b7 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b8 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b9 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b10 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b11 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b12 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b13 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b14 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSA Space Proc Flow Mon b15 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSB HV Swp Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB HV Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB Spectra Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB Time Tag Cmd TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB RTMD A Sense TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB RTMD B Sense TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB FDR1 Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSB FDR2 Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:49 1992-08-07 12:00:03 TSS : TSS-1 : SPREE : SPREE : SPSC FDR1 Filemark TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR1 Begin or EOT TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR1 CTS TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR1 Pwr Fail/Rec TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR1 Sense Key TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR2 Filemark TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR2 Begin or EOT TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR2 CTS TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR2 Pwr Fail/Rec TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSC FDR2 Sense Key TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : SPREE : SPREE : SPSD DCORE/SETS Gun Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DCORE and SETS gun status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1992-08-02 07:37:44 1992-08-07 12:00:00 TSS : TSS-1 : TEMAG : TEMAG : TMHA Out/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA In/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA Ele/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA -8V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA +12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA -12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA +5V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHA Spare TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHB TeleCmd Echo TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMHB Chksum TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMI In/Bx TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMI In/By TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMI In/Bz TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMO Out/Bx TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMO Out/By TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMMO Out/Bz TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1 : TEMAG : TEMAG : TMTA Tether Cur. TSS:TSS-1:TEMAG:TEMAG:TMTA This virtual contains the tether current data obtained from the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor all 0,1 0,0 mamps Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Tether Current Obtained from the Satellite Ampmeter 8 1992-08-03 03:38:34 1992-08-05 10:59:32 TSS : TSS-1R : CAS : CAS : CSAA IMU Body Rate X TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA IMU Body Rate Y TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA IMU Body Rate Z TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Q-M50 To Body Ele1 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Q-M50 To Body Ele2 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Q-M50 To Body Ele3 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Q-M50 To Body Ele4 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Q-M50 To Body Time TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA M50 (LV,LH) Q1 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA M50 (LV,LH) Q2 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA M50 (LV,LH) Q3 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA M50 (LV,LH) Q4 TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Roll Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Pitch Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Yaw Error TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Shuttle Alt TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Cur Apogee TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAA Cur Perigee TSS:TSS-1:CAS:CAS:CSAA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point. The following is a list of tables which are in this vidf TABLE 0: unit conversions The following table lists the sensor units as stored SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------- ------------------------ 0 degrees/sec | 1 degrees/sec | 2 degrees/sec 3 unitless | 4 unitless | 5 unitless 6 unitless | 7 seconds | 8 unitless 9 unitless | 10 unitless | 11 degrees 12 degrees | 13 degrees | 14 degrees 15 feet | 16 nautical miles | 17 nautical miles The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition SENSORS TABLES OPERS UNIT 15, 16, 17 0 0 kilometers Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur XPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur YPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur ZPos TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur XVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur YVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Fltrs Cur ZVel TLM TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target XPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target YPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target ZPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target XVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target YVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Cur Target ZVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Target XAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Target YAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Target ZAcc TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar XPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar YPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar ZPos TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar XVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar YVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Rel Orb/Tar ZVel TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Last Tar Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Last State Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSAB Filter State Update Tm TSS:TSS-1:CAS:CAS:CSAB This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 feet | 1 feet | 2 feet 3 feet/sec | 4 feet/sec | 5 feet/sec 6 feet | 7 feet | 8 feet 9 feet/sec | 10 feet/sec | 11 feet/sec 12 feet | 13 feet | 14 feet 15 feet/sec | 16 feet/sec | 17 feet/sec 18 feet/s**2 | 19 feet/s**2 | 20 feet/s**2 21 seconds | 22 seconds | 23 seconds The following table is included in the VIDF TABLE 0: conversion factor taking feet to meters The following are units which can be derived from the table. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2,6-8,12-14 0 3 meters Sweep 3-5,9-11,15-17 0 3 meters/sec Sweep 18-20 0 3 meters/sec**2 Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Shuttle Lat TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Shuttle Long TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Pitch (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Yaw (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Roll (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Pitch Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Yaw Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Roll Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Sat Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Sat Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Ram Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Ram Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCA Orbit # TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCB FES Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCB Water Dump Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSCB Thruster Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS LT BL T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS RT BL T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS LT BL T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS RT BL T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS L Sill Longn T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS L Sill Longn T@1030 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS L Sill Longn T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS R Sill Longn T@650 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS R Sill Longn T@1030 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA M-FUS R Sill Longn T@1215 TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 1 Evap Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 2 Evap Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 1 Rad Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 2 Rad Outlet T TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 1 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 2 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 3 V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 1 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 2 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA FCL 3 I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA Mid PCA Main Bus A I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA Mid PCA Main Bus B I TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA P/L Pri Main Bus B V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEA P/L Pri Main Bus C V TSS:TSS-1:CAS:CAS:CSEA This virtual contains the shuttle temperature, voltage and current monitors. Data includes M-FUS and FCL temperatures, fuel cell voltages and currents, and some of the bus currents and voltages. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-13 to degrees F, from sensors 14-16, 22-23 to volts and from sensors 17-21 to amps TABLE 1: conversion of degrees F to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 degrees F Sweep 0-13 0,1 0,0 degrees C Sweep 14-16 0 0 volts Sweep 22-23 0 0 volts Sweep 17-21 0 0 amps Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEB Sup H2O Tank A Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEB Sup H2O Tank B Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEB Sup H2O Tank C Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEB Sup H2O Tank D Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSEB Waste H2O Tank Quan TSS:TSS-1:CAS:CAS:CSEB This virtual contains the shuttle supply and waste water monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to percent The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 percent Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 Roll Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 Pitch Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 DES Roll Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 DES Pitch Wd TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 Rng Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 Roll Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMA KU-A CH1 Pitch Rate TSS:TSS-1:CAS:CAS:CSMA This virtual contains the KU Band A word monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to degrees, from sensor 4 to feet/sec, and from and from sensors 5-6 to degress/sec. TABLE 1: sign (+/-) of converted sensor data TABLE 2: conversion of feet to meters The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0,1 0,3 degrees Sweep 4 0,1 0,3 feet/sec Sweep 4 0,1,2 0,3,3 meters/sec Sweep 5-6 0,1 0,3 degrees/sec Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 4 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMB KU-A CH1 Radar Rng TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMB KU-A CH1 Targ Rng Est TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSMB KU-A Comm Radar RF Pwr TSS:TSS-1:CAS:CAS:CSMB This virtual contains the KU Band A range and power monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to kilofeet and from sensor 2 to watts. TABLE 1: conversion from kilofeet to kilometers The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,1 0 0 kilofeet Sweep 0,1 0,1 0,3 kilometers Sweep 2 0 0 watts Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Fuel Cell Auto Purge TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 1 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 2 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 3 Purge V MNL TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 1 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 2 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA FCP 3 Purge V GPC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Suply H20 Dmp ISLN V TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Suply H20 Dmp Valve TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Waste H20 Dmp ISLN V TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Waste H20 Dmp Valve TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Flash Evap Cntrl Pri A-GPC CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Flash Evap Cntrl Pri B-GPC CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Flash Evap Cntrl Pri A CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA Flash Evap Cntrl Pri B CMD TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA PL Pri Main B Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSA PL Pri Main C Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the CAS FCP and Water dump valve status as well as the Payload Primary power status. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A RADAR Pass Mode TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A RADAR Out-Med TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A RADAR Out-Hi TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Comm A/RDR Mode TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Anten Strg Auto TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Anten Strg GPC DES TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Anten Strg GPC AGC TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Rng Data TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB KU-A CH1 Rng Rate TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB GCIL KU-A Pwr TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB Rec Ops1 Tape Motion TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSB Rec Ops2 Tape Motion TSS:TSS-1:CAS:CAS:CSSA This virtual contains the KU-Band Communications/Radar and recorder operation status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F1F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F1L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F1D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F2F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F2R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF1 Jet F2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F3F TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F3L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F3U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F4R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F5L Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDF2 Jet F5R Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L1A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L1L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L2L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R1A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R1R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R1U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R2R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R2U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet R2D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L5D Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA1 Jet L5L Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L3A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L3L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L4L TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L4U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet L4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R3A TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R3R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R3D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R4R TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R4U TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R4D TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R5R Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSSC RJDA2 Jet R5D Vernier TSS:TSS-1:CAS:CAS:CSSA This virtual contains the RCS/Vernier and Jet-Impulse/Exhaust status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions or sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted GMT Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted GMT Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted GMT Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted GMT Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted GMT Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted MET Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted MET Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted MET Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted MET Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM Voted MET Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted GMT Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted GMT Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted GMT Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted GMT Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted GMT Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted MET Day TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted MET Hr TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted MET Min TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted MET Sec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : CAS : CAS : CSTA MTU-PCM NonVoted MET Msec TSS:TSS-1:CAS:CAS:CSTA This virtual instrument contains the orbiter and target state vectors. The data is stored as floating point values and are already in the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 days | 1 hours | 2 minutes 3 seconds | 4 milliseconds | 5 days 6 hours | 7 minutes | 8 seconds 9 milliseconds | 10 days | 11 hours 12 minutes | 13 seconds | 14 milliseconds 15 days | 16 hours | 17 minutes 18 seconds | 19 milliseconds | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 09:26:29 1996-03-01 11:00:00 TSS : TSS-1R : DCORE : DCORE : DCDV DV/Autochk TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCDV DV/Voltage TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCDV DV/Autochk Active TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCDV DV/Overflow TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCDV DVG Pressure TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA1 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA2 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA1 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA2 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA1 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA2 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA1 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA2 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA1 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGA EGA2 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGB EGA1 Offset I TSS:TSS-1:DCORE:DCORE:DCGB This virtual contains the DCORE EGA offset current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to millamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGB EGA2 Offset I TSS:TSS-1:DCORE:DCORE:DCGB This virtual contains the DCORE EGA offset current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to millamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGC EGA1 Acc Poten TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGC EGA2 Acc Poten TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGC EGA1 Fila V TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCGC EGA2 Fila V TSS:TSS-1:DCORE:DCORE:DCGC This virtual contains the DCORE EGA filament voltages and the acceleration potentials The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Analog Ref Mon1 TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Analog Ref Mon2 TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Masked Units Buf TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Health Status TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA TLC Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Configuration TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Remaining Seq TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Remaining Pul TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Rep Cmd Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMA Rep Mon Cntr TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains some general DCORE monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 volts-dc Sweep 2-9 counts Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Op Sys Warning B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Op Sys Warning B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Op Sys Warning B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CV Rpt Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CV Rpt Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CV Rpt Buf B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CV Rpt Buf B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CA Rpt Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB CA Rpt Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Masked Mon Buf B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Prgm Status B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Prgm Status B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Prgm Status B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Prgm Status B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B1 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B2 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B3 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Fault Mon Stat B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dump Add B4 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dump Add B5 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area2 B6 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area2 B7 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area3 B8 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area3 B9 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area4 B10 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area4 B11 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area5 B12 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area5 B13 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area6 B14 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB DCORE Dmp Area7 B15 TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMB Mon Error Val TSS:TSS-1:DCORE:DCORE:DCMB This virtual contains the DCORE memory dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA1 Fila I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA1 Fila I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA2 Fila I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA2 Fila I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA1 Tether I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA1 Tether I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA2 Tether I Cyc2 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMC EGA2 Tether I Cyc6 TSS:TSS-1:DCORE:DCORE:DCMC This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-3 to amps and from sensors 4-7 to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 amps Sweep 4-7 0 0 milliamps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Fmt Cntr TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Mem Addr TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Dmp Area2 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Dmp Area3 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Dmp Area4 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Dmp Area5 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCMD DCORE Dmp Area6 TSS:TSS-1:DCORE:DCORE:DCMD This virtual contains the DCORE dump data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm1 bits(0-31) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm1 bits(32-63) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm1 bits(64-95) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm2 bits(0-31) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm2 bits(32-63) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCME Apl Prgm2 bits(64-95) TSS:TSS-1:DCORE:DCORE:DCME This virtual contains the DCORE active programs monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA EGA1 Filament TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA EGA2 Filament TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA EGA1 High Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA EGA2 High Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA DV Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA CWGHS Swtch 1 TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA CWGHS Swtch 2 TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA CWGHS Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA DV Pwr TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA DV Hi Volt Swtch TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSA DV Autochk TSS:TSS-1:DCORE:DCORE:DCSA This virtual contains the high temporal resolution EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA1 Filament TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA1 HiPwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA1 Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA1 HiPwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA1 Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA2 Filament TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA2 HiPwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA2 Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA2 HiPwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EGA2 Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Swtch 1 TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Swtch 2 TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Swtch 1 Ver TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB CEGHS Swtch 2 Ver TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DV Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DV Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DV HV Swtch TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DV AutoChk TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DV Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DVG Pwr TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DVG Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DVG Pwr Line TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB PDECU Unit TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB EOFF Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB QPM Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB PICV Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB STB Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB SIVC/LFCP Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB IDLE Mode TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB DCORE ChkOut TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB Exe ChkOut TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB Trans Seq Go/Nogo TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCSB Trans In Prog TSS:TSS-1:DCORE:DCORE:DCSB This virtual contains EGA and Digital voltimeter status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA1 Fluid T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA2 Fluid T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA1 Head T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA2 Head T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA1 Fila PS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA2 Fila PS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA1 Coil T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA2 Coil T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA DVG T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA CEGHS T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA DV T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA1 Xfomer T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA EGA2 Xfomer T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA PDECU T1 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA PDECU T2 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA PDECU T3 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA PDECU T4 TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DCORE : DCORE : DCTA DVG DDCU T TSS:TSS-1:DCORE:DCORE:DCTA This virtual contains the DCORE temperature monitor data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 09:33:34 1996-03-01 11:00:29 TSS : TSS-1R : DPLY : DPLY : DPHA SFMDM Cmd Cnt TSS:TSS-1:DPLY:DPLY:DPHA This virtual contains miscellaneous deployer housekeeping monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry for sensor 1 to integer The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHA Cmded Pwidth TSS:TSS-1:DPLY:DPLY:DPHA This virtual contains miscellaneous deployer housekeeping monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry for sensor 1 to integer The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd00 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd01 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd02 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd03 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd04 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd05 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd06 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd07 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd08 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd09 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd10 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd11 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd12 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd13 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd14 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd15 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd16 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd17 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd18 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd19 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd20 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd21 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd22 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd23 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd24 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd25 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd26 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd27 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd28 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHB SFMDM Cmd Wd29 TSS:TSS-1:DPLY:DPLY:DPHB This virtual contains the SFMDM command words. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Offset TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Seg TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd00 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd01 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd02 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd03 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd04 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd05 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd06 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd07 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd08 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd09 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd10 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd11 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd12 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Rot Mem Dmp Wd13 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC ROM Chksum TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC Invalid Int Cnt TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHC RAM Chkout Fails TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains the rotating memory dump data words together with some of the RAM and ROM monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHD Cur Seg Num In Prof TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHD % Time Ellapsed TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHD Time Remain TSS:TSS-1:DPLY:DPLY:DPHD This virtual contains the segment monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to percentage and form sensor 2 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 - - integer Sweep 1 0 0 percentage Sweep 2 0 0 seconds Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHE Time Stmp TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHE Time Stmp Frm1 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPHE Time Stmp Frm2 TSS:TSS-1:DPLY:DPLY:DPHC This virtual contains time stamp data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMA CP Outbd Fine Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMA CP Outbd Coar Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMA CP Inbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMA This virtual contains the CP tether tension monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Outbd Blended Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Cmded Outbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB 8Bit Inbd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB % Basic Ctrl Mode TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Cmded Tether Acc TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Cmded Libra Vel TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Cmded Libra Ang TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Blended Ten Filt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Tether Len Filt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB REG V/Prop Ctrl TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMB Reg/Volt TSS:TSS-1:DPLY:DPLY:DPMB This virtual contains the low temporal resolution tether monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to newtons for sensors 0-2, to percentage for sensor 3, to m/s**2 for sensor 4, to m/s for sensor 5, to degree for sensor 6, and to volts for sensors 7-10 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2 0 0 newtons Sweep 3 0 0 percentage Sweep 4 0 0 m/s**2 Sweep 5 0 0 m/s Sweep 6 0 0 degrees Sweep 7,10 0 0 volts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMC Unstrtch Tether Len TSS:TSS-1:DPLY:DPLY:DPMC This virtual contains the measured tether length and rate. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters for sensor 0 and m/s for sensor 1 TABLE 1: polynomial coefficients taking telemetry to km for sensor 0 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 meters Sweep 0 1 0 km Sweep 1 0 0 meters/secs Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMC Tether Rate TSS:TSS-1:DPLY:DPLY:DPMC This virtual contains the measured tether length and rate. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters for sensor 0 and m/s for sensor 1 TABLE 1: polynomial coefficients taking telemetry to km for sensor 0 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 meters Sweep 0 1 0 km Sweep 1 0 0 meters/secs Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMD Tether Rate Raw Tmr Cnts TSS:TSS-1:DPLY:DPLY:DPMD This virtual contains the tether rate raw timer counts data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Ctrl Law Param 00 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Estimated Reel Rad TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Strtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded UnStrtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Spooled UnStrtched Tether Len TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Spool Tether Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded In-Pl Libr Ang Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Est Reel Motor Ang Vel TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Acc TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded In-Pl Libr Ang Acc TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Outbd Tension TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Outbd Blended Tension TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Elapsed Manu Time TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Motor/Gen Pulsewidth TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Load Res TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded Reel Motor Ter V TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Ctrl Law Param 12 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Ctrl Law Param 18 TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cur Seg Dur Time TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cur Seg Init Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cur Seg End Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cur Seg Type TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPME Cmded In-Pl Libr Ang TSS:TSS-1:DPLY:DPLY:DPME This virtual contains many of the commanded tether and tether monitors. All of data is stored in floating format, and is already in physical units. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to km for for sensors 1-4 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,17,18 - - integer Sweep 1-4 - - meters Sweep 1-4 0 3 km Sweep 5-6 - - m/s Sweep 7-8 - - radians/s Sweep 9 - - m/s**2 Sweep 10 - - radians/s**2 Sweep 11-12 - - newtons Sweep 13,19 - - seconds Sweep 14,22 - - counts Sweep 15 - - ohms Sweep 16 - - volts Sweep 20,21 - - degrees Sweep 23 - - radians Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Latch Gr1 Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Latch Gr2 Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Boom Motors I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF MCA-Reel Motor I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sat Bat Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sat P/L Mod Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sat Serv Mod Htr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF MPC-MCA I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF MPC Input I Hi Rng TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF MPC Input I Low Rng TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sat Ext Pwr I TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF MCP V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sat Ext Pwr V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Pri Upper Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Pri Lower Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Pri Boom Eject V1 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Pri Boom Eject V2 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Pri Boom Eject V3 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sec Upper Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sec Lower Tether Cut V TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sec Boom Eject V1 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sec Boom Eject V2 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Sec Boom Eject V3 TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Outbrd Fine Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Outbrd Coarse Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMF Inbrd Tether Ten TSS:TSS-1:DPLY:DPLY:DPMF This virtual contains miscellaneous current and voltage monitors together with tether tension data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-10, to volts for sensors 11-22 and to newtons for sensors 23-25 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 amps Sweep 10-22 0 0 volts Sweep 23-25 0 0 newtons Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMG Mea Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMG Cmded Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMH Mea Tether Vel TSS:TSS-1:DPLY:DPLY:DPMH This virtual contains the commanded and measured tether velocity monitors. The tether velocity is spread out over the sensors and two calibration sets. The sensor holds the integer portion of the velocity, cal set 0 the fractional part and cal set 1 the sign. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meter/sec TABLE 1: polynomial coefficients cal set 1 sign of velocity The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 3 meters/sec Cal 0 0 0 meters/sec Cal 1 1 0 sign Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMH Cmded Tether Vel TSS:TSS-1:DPLY:DPLY:DPMH This virtual contains the commanded and measured tether velocity monitors. The tether velocity is spread out over the sensors and two calibration sets. The sensor holds the integer portion of the velocity, cal set 0 the fractional part and cal set 1 the sign. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meter/sec TABLE 1: polynomial coefficients cal set 1 sign of velocity The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 3 meters/sec Cal 0 0 0 meters/sec Cal 1 1 0 sign Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMI Tether Len Raw Enc Cnts TSS:TSS-1:DPLY:DPLY:DPMI This virtual contains the tether length raw encoder counts data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMJ Meas DEL-L Cir1 TSS:TSS-1:DPLY:DPLY:DPMJ This virtual contains the tether DEL-L measurements. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters TABLE 1: polynomial coefficients taking telemetry to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 meters Sweep all 1 0 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMJ Meas DEL-L Cir2 TSS:TSS-1:DPLY:DPLY:DPMJ This virtual contains the tether DEL-L measurements. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to meters TABLE 1: polynomial coefficients taking telemetry to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 meters Sweep all 1 0 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPMK Reel Motor Cmd (Pwdth) TSS:TSS-1:DPLY:DPLY:DPMK This virtual contains the reel motor command (pulsewidth) There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/counts Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA 0% Boom Retr 1 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA 0% Boom Retr 2 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA 100% Boom Exten 1 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA 100% Boom Exten 2 TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Exten Mode TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Retr Mode TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Motor Sel TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Motor Dir Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Motor A ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Boom Motor B ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSA Enable InterBoom Stop Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSA This virtual contains the satellite boom status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC MCA Pwr TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC JTS Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC JTS Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC DPY/RTR Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC DPY/RTR Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Sat Int Pwr HARD TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Sat Int Pwr DBuf TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Sgl Ended ADC V1 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Sgl Ended ADC V2 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Diff ADC V1 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSC Diff ADC V2 TSS:TSS-1:DPLY:DPLY:DPSC This virtual contains the deployer power status and ADV voltage monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 1 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 2 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 3 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 4 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 5 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch 6 Closed TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch Grp1 Open TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch Grp2 Open TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Open Latch Grp1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Open Latch Grp2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Close Latch Grp1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Close Latch Grp2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch Open Dir Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch Open Enable TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD Latch Open Dir TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSD At Least 4 Latches Clsd TSS:TSS-1:DPLY:DPLY:DPSD This virtual contains the deployer latch status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Sep Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Spare1 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Spare2 Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Retract 1 TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Full Retract 3 TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Sep TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U1 Sep Pwr TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U2 Sep Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U2 Sep TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSE U2 Sep Pwr TSS:TSS-1:DPLY:DPLY:DPSE This virtual contains the deployer U1 and U2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Cir1 Sec TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Cir1 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Cir2 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Cir2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Disable1 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF L-DOT Disable2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF DEL-L Cir1 Sec TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF DEL-L Cir1 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF DEL-L Cir2 Trig TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF DEL-L Cir2 TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF Tklbk Status TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSF Tklbk Mon TSS:TSS-1:DPLY:DPLY:DPSF This virtual contains the deployer L-DOT, DEL-L and talkback status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG MPC TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG MPC VCMD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG JTS Enable HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG JTS Enable D-Buf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG JTS Fire HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG JTS Fire D-Buf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG DPY/RTR Enable HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG DPY/RTR Enable DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG DPY/RTR Status HARD TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG DPY/RTR Status DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Gyro Status DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG OBDH SlfChk DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG RAM Chkout TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG ROM Chkout TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Sat InLn Thrus DACA TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Sat InLn Thrus Nec TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Sat Hunt Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Sat TLM Buf Full TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Update Par Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Brake Sen Under V1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Brake Sen Under V2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Reel Lock Diseng2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Torq Test1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Torq Test2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Prop/Basic Ctrl Mode TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG St Const PW Ret Enabled TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Ctrl Laws Active TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Inst Tether Dir1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Inst Tether Dir2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Motor/Gen Enable TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Resis Bank1 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Resis Bank2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Reel Motor Enable TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Torq Test Cmd2 TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG APS Pres DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Bat Temp DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSG Gyro Temp DBuf TSS:TSS-1:DPLY:DPLY:DPSG This virtual contains miscellaneous deployer status monitors which are returned at a rate of 1 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH DACA Rdy For Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH DACA Cmd Auth TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH DACA Cmd Exe Suc TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH TLM Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH StaKping Man Hold TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH On Sta Status TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH TmOut Abort TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH Nom Cmd Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSH Motor/Gen Mode TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer status monitors which are returned at a rate of 16 per major frame. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSI SoftStop Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSI Resume To Sta1 Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSI Resume To Sta2 Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSI Resume To Dock Man Req TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSI SoftStop Man Exe TSS:TSS-1:DPLY:DPLY:DPSI This virtual contains the deployer maneuver status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Crit Func Relay Status TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Crit Func Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Ver Motor Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Ver Motor Clu Eng Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Ver Motor Rmpdwn Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ MCA Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ TT&C Pwr On Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Sat Bat Htrs Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Sat Ext Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Sat Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Dply Rly Rest Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Hot Nest Pwr Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ MPC ON Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ MPC VCMD Hi Rly Cmd TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPSJ Crit Func Rly Cmp TSS:TSS-1:DPLY:DPLY:DPSH This virtual contains miscellaneous deployer relay status monitors The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Mo Cld Plate T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Cvr T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Bearing Hs1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Bearing Hs2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Brake Motor T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Motor1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Reel Motor2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Boom Motor1 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Boom Motor2 T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Boom Motor1 Ele T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTA Boom Motor1 Ele T TSS:TSS-1:DPLY:DPLY:DPTA This virtual contains the deployer reel and boom temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 1 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 2 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 3 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 4 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 5 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Latch 6 Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Dock Ring Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Lnch Lock Diseng Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Load Bank 1 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Load Bank 2 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Load Bank 3 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Load Bank 4 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Struc Struts T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Struc Struts T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Sat Sup Struc T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Sat Sup Struc T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB DACA-PICA Cld Plate 5 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB MCA Cld Plate 6 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB MPC Cld Plate 10 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB LTCM Load Cell T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB LTCM Encoder T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Pallet T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Pallet T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB HVRA T1 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB HVRA T2 TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB PICA 1 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB PICA 2 T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB MCA T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB DACA T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB UTCM Struc T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Ver Motor T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB Ver Motor Ele T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DPLY : DPLY : DPTB MPC T TSS:TSS-1:DPLY:DPLY:DPTB This virtual contains miscellaneous deployer temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 1 1996-02-22 11:51:19 1996-03-01 10:51:19 TSS : TSS-1R : DRB : DRB : DBPO DRBA Header TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBPO DRBA Tip Pos TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBPO DRBD Header TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBPO DRBD Tip Pos TSS:TSS-1:DRB:DRB:DBPO This virtual consists of status monitors and lengths of the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking the telemetry from sensors 1 and 3 to millimeters TABLE 1: ascii definitions of states of sensors 1 and 3 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 1,3 0 0 millimeters Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBA Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBA Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBA P/L Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBA P/L Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBD Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBD Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBD P/L Main Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DRBD P/L Red Stowed TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA DPY/RTR Enable TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSA JTS Enable TSS:TSS-1:DRB:DRB:DBSA This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBA Stow SW Main:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBA Stow SW Main:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBA Stow SW Red:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBA Stow SW Red:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBD Stow SW Main:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBD Stow SW Main:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBD Stow SW Red:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DRBD Stow SW Red:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB Motor:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB Motor:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB CPU Watchdog:1 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB CPU Watchdog:2 TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB DPT/RTR TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSB JTS Fire TSS:TSS-1:DRB:DRB:DBSB This virtual consists of some of the event flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSC DPY/RTR Pwr TSS:TSS-1:DRB:DRB:DBSC This virtual consists of the power monitor flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBSC JTS Pwr TSS:TSS-1:DRB:DRB:DBSC This virtual consists of the power monitor flags for the Deployable Retrievable Booms (DRB) The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBTA DRBA Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBTA DRBD Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : DRB : DRB : DBTA DRBE Temp TSS:TSS-1:DRB:DRB:DBTA This virtual contains the DRB temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C Jean Sabbagh ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : EMP : EMP : EPMA EMP PCB T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP SFMDM Pri Core T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP SFMDM Sec Core T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Freon Pmp Out T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Freon Inlet T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Exp Freon Ret T TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Pallet Struc T1 TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Pallet Struc T2 TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA DMS Temp TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Exp DC V TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Exp DC Cur TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Freon Pmp Inlet Pres TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Freon Pmp Dlta Pres TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMA EMP Freon Pmp Acc Quan TSS:TSS-1:EMP:EMP:EPMA This virtual contains some of the pallet temperature, voltage, current and freon monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-8 to degrees F, from sensor 9 to volts, from sensor 10 to amps, from sensors 11-12 to psi, and from sensor 13 to cubic-ft The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-8 0 0 degrees F Sweep 9 0 0 amps Sweep 10 0 0 volts Sweep 11-12 0 0 psi Sweep 13 0 0 cubic foot Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 1 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 1 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 2 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 2 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 3 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 3 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 4 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 4 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 5 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 5 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 6 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 6 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 7 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 7 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 8 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 8 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 9 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 9 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 10 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 10 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 11 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 11 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 12 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 12 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 13 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 13 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 14 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 14 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 15 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 15 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 16 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB OCB 16 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB Type TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB Off In File TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 2 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 2 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 3 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 3 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 4 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 4 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 5 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 5 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 6 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 6 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 7 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 7 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 8 Pt1 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMB VDB 8 Pt2 TSS:TSS-1:EMP:EMP:EPMB This virtual contains the EMP output command block and variable data block data There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B1 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B2 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B3 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B4 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B5 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B6 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B7 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B8 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B9 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B10 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B11 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B12 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B13 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B14 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B15 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B16 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B17 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B18 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B19 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B20 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B21 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B22 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B23 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B24 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B25 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B26 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B27 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B28 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B29 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B30 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B31 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B32 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B33 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMC SFMDM Last Acc Cmd B34 TSS:TSS-1:EMP:EMP:EPMC This virtual contains the last accepted command buffer for the SFMDM There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF No TECS in Buf TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF GMT-Nxt TEC to Exec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Lst Cmd Exec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Master Exec Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Sub Exec Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Entry # of Lst Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Eff GMT of Lst Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF DDCS MF Cntr TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C5 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C6 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C7 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Fname C8 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Exten C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Exten C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF TmLine Exten C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Master C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Master C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Master C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Master C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Master C5 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Sub C1 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Sub C2 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Sub C3 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Bkgnd Sub C4 TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF DDCS GMT-Day TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF DDCS GMT-Sec TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF DDCS RS422 Sync Stat TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF No Of Invald Uplnk Cmd TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF DDCS Sys Perf TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMF Dsply No Sel TSS:TSS-1:EMP:EMP:EPMF This virtual contains the timeline data. The following is a list of tables which are in this vidf TABLE 0: Ascii state definitions for sensors 3-27 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-27,30-33 hex/integer Sweep 28 day Sweep 29 seconds Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Inpt Cmd Cntr TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Byte Cmd In Prog TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Core Swtch Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Sync Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Tele Fmt TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Fmt Id TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Cmd Rej Cnt TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Patch Cntr TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Pwr Fail TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM FVOS Err TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SFMDM Byte Err Code TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG EMP Byte Stat Reg TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG I/O Xfer TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG SDIO Acq Cmd FdBk TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Pri/Bkup Core Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG EMP Byte Cmd Ind TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG EPROM Patch Test Sel TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG RAM Chksum TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMG Parser On Hold TSS:TSS-1:EMP:EMP:EPMG This virtual contains miscellaneous monitors and SFMDM data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMH SFMDM RS-422 # of Bits TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMH SFMDM RS-422 Parity TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMH SFMDM RS-422 BaudRate TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMH SFMDM IO Xfer IOM Inpt Err TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPMH SFMDM IO Xfer # of Errs TSS:TSS-1:EMP:EMP:EPMH This virtual contains SFMDM RS-422 and I/O transfer data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DMS Switch 1 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DMS Switch 2 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA EGA1 HP Enable TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA EGA2 HP Enable TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-EGA1 HP Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-EGA2 HP Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-EGA1 Coil Cur Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-EGA2 Coil Cur Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-DV +5V Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-DV Volt Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-DV Ovrflw Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pre-DVG Pres Out Of Lim TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Dply Htr Pwr (K2) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DACA Pwr (K3) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Dply Pri Func Pwr (K4) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Sat Htrs/Cmd Pwr (K5) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Dply Sec Func Pwr (K6) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Sat Quies Htr Pwr (K7) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA EMP DC Pwr (K8) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA MPC Pwr (K9) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA EMP AC Pwr (K12) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pallet Cool Sys Pri Pwr (Pmp1) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Pallet Cool Sys Pri Pwr (Pmp2) TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA MCP OCP Setpnt TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA SPREE Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DCORE Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA SETS Pwr TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA RTMD A TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA RTMD B TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA FDR 1 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA FDR 2 TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA MCP A TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA MCP B TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Defl Plate A V TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA Defl Plate B V TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DDCU Tmline Mod TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSA DDCU GMT Mode TSS:TSS-1:EMP:EMP:EPSA This virtual contains the pallet satellite and deployer status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg PS Byte Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg Int Bus TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg Data !Xfer TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg Ch !Pres TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg BSDIO Mod Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM EReg Pwr Int Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM GMT Invld TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM UART Frm Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM UART Ovrn Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM UART Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM UART Byte Mode Req TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS422 Stop Bit TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer Int Bus Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer Data !Xfer TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer Ch !Pres TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer !Suc TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM IO Xfer Re-EXEC Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR EPROM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR RAM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR ADC Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR CPU Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR APU Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR Mem Mod Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR Pwr Sup Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DCO Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR SDIO Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DO5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR RS422 SI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR PO5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DI5 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR RIOUM1 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR RIOUM2 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DCIN Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR PO28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DO28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DI28 Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR GMTI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR DLM Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR PRGI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM BSR PSPI Byte Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Mon Enab TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Ext Inpt TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Frm Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Ovrn Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Parity Err TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Xfer Buf Emp TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM RS232 SW Data Rec TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Pri Core Act TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Bkup Core Act TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Othr Core Fail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Parbuf Unavail TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Prsr Rej Cmd TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Sync Loss w/DDCU TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Invld Sync/Sour TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Invld IOM/CMD Id TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Invld Chksum TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSB SFMDM Maint Wd Cnt TSS:TSS-1:EMP:EMP:EPSB This virtual contains SFMDM status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch00 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch01 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D05 Ch02 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L0 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L1 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L2 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L3 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L4 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L5 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L6 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L7 Lev TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch00 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch01 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/U7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L0 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L1 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L2 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L3 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L4 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L5 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L6 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSC SFMDM D28 Ch02 B/L7 Pul TSS:TSS-1:EMP:EMP:EPSC This virtual contains SFMDM status monitors. There are no tables associated with this vidf Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch00 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch00 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch01 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch01 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch02 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch02 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch03 Act TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : EMP : EMP : EPSD SDIO Ch03 Rec TSS:TSS-1:EMP:EMP:EPSD This virtual contains the SDIO channel status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-22 11:05:04 1996-03-01 11:01:41 TSS : TSS-1R : RETE : RETE : RTEF DC-EF: (V1-V2) TSS:TSS-1:RETE:RETE:RTEF The RETE Langmuir probe DC, 0-2 Hz, electric field measurements. For these measurements the two dipole probes are run either in the biased or unbiased state (at one of 3 different current values). The states are selected by telecommand. In addition the probes can be set by telecommand to be in a high or low gain state. The default state is no bias, low gain. The sampling rate depends on the instrument mode (5/sec in NM, and 32/sec in PP2). The following is a list of tables which are in this vidf TABLE 0: Lookup tables converting telemetry to volts for both high and low gain TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTFP Langmuir/I TSS:TSS-1:RETE:RETE:RTFP This data is acquired from the Langmuir probe with the probe biased as a fixed potential. The probe potential is stored in the scan index. This makes this vidf a vector instrument of length 1. The following is a list of tables which are in this vidf TABLE 0: Langmuir probe current (amps) TABLE 1: Fixed Potential (volts) TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 volts Sweep 4 0 amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-24 12:59:23 1996-02-25 08:59:16 TSS : TSS-1R : RETE : RETE : RTHF Ex TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTHF Ey TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTHF Ez TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTHF Bx TSS:TSS-1:RETE:RETE:RTHF This virtual contains the RETE AC high frequency electromagnetic wave data. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * 10**{(C2J*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands This instrument had no associated digital spectrum analyzer as do the low and medium frequency band analyzers and so the computation of N is suppressed. What is returned in the telemetry sweep data are the AGC values for each frequency step. The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table for telemetry giving 10**(C1*AGC/10) TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 4: lookup table for cal set 0 giving 10**{(C2*att+C3)/10} The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-3 1,2,3 0,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTIP Ion Probe I TSS:TSS-1:RETE:RETE:RTIP The RETE ion probe current. The sensor is a simple electrostatic ion trap (Faraday Cup), biased at a fixed voltage of -7.5V with respect to the canaster. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting telemetry to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 amps Sensor 0 1 0 nanoamps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 05:00:13 TSS : TSS-1R : RETE : RETE : RTKA WRA Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA DPU Int Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA ACDP Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA DCE Temp TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA RETE I TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA Synth Ctrl V TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +5V DCE TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +15V DCE TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA -15V DCE TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +6V WRA Dig Filters TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA -6V WRA TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA -18V WRA TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +6V WRA TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +5V DPU TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA +12V DPU TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA -12V DPU TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKA Ref Supply TSS:TSS-1:RETE:RETE:RTKA This virtual contains the RETE AC housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry from sensors 0-3 to degrees C and sensor 4 to amps; polynomial coefficients taking telemetry from sensors 5-16 to volts TABLE 1: polynomial coefficients taking cal set 0 telemetry to volts (voltage corrections for sensors 8, 10, 11) Note: sensor 3 (DCE Temp) scaling updated from TSS-1 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4 0 0 amps Sweep 4-7,9,12-16 0 0 volts Sweep 8,10-11 0,1 0,1 volts Cal 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Ram Add Line TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Checksum TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Exceeding Data TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Overrun TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Framing TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Parity TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC HF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC MF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC LF TimeOut TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKC Exceeding Samp TSS:TSS-1:RETE:RETE:RTKC This virtual contains the RETE error table monitors The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKD TeleCmd Echo TSS:TSS-1:RETE:RETE:RTKD This virtual contains the RETE telecommand echo. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKE Pentode/I TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKE DCBP/Pot TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKF RETE Mode TSS:TSS-1:RETE:RETE:RTKF This virtual contains the RETE format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 05:59:57 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKF RETE Pg# TSS:TSS-1:RETE:RETE:RTKF This virtual contains the RETE format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 05:59:57 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKG LF Mode TSS:TSS-1:RETE:RETE:RTKG This virtual contains the RETE LF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTKG LF Sens TSS:TSS-1:RETE:RETE:RTKG This virtual contains the RETE LF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTKH MF Input 1 Sens TSS:TSS-1:RETE:RETE:RTKH This virtual contains the RETE MF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the sensor telemetry There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKH MF Input 2 Sens TSS:TSS-1:RETE:RETE:RTKH This virtual contains the RETE MF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the sensor telemetry There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKI HF Mode TSS:TSS-1:RETE:RETE:RTKI This virtual contains the RETE HF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTKI HF Sens TSS:TSS-1:RETE:RETE:RTKI This virtual contains the RETE HF format data The following is a list of tables which are in this vidf TABLE 0: ascii definitions of the telemetry of sensor 0 There are no tables which alter the sensor units. The sensor units as exists in the telemetry are given below DATA TYPE SENSOR UNIT Sweep all integer/hex Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:15 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTLA Ex TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTLA Ey TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTLA Ez TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTLA Bx TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTLA Bz TSS:TSS-1:RETE:RETE:RTLA This virtual contains the RETE AC electromagnetic wave data from band A in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 3 1996-02-23 05:59:57 1996-03-01 05:39:28 TSS : TSS-1R : RETE : RETE : RTLB Ex TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1996-02-23 06:00:06 1996-03-01 05:39:38 TSS : TSS-1R : RETE : RETE : RTLB Ey TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1996-02-23 06:00:06 1996-03-01 05:39:38 TSS : TSS-1R : RETE : RETE : RTLB Ez TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1996-02-23 06:00:06 1996-03-01 05:39:38 TSS : TSS-1R : RETE : RETE : RTLB Bx TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1996-02-23 06:00:06 1996-03-01 05:39:38 TSS : TSS-1R : RETE : RETE : RTLB Bz TSS:TSS-1:RETE:RETE:RTLB This virtual contains the RETE AC electromagnetic wave data from band B in the low frequency range. The experiment measures the electric field fluctuations along all three principle axes. Thei x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. The data are converted to physical units through the algorithm: E = 10**{C1*AGC/10} * N * 10**{(C2*atten + C3)/10} * 10**{C0/10} where: E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup table decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} TABLE 5: ascii definitions for cal set 2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep all 1,2,3,4 0,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 2 1996-02-23 06:00:06 1996-03-01 05:39:38 TSS : TSS-1R : RETE : RETE : RTMC Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMC Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMC This virtual contains the RETE AC electromagnetic wave data from band C in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:48 1996-03-01 04:59:40 TSS : TSS-1R : RETE : RETE : RTMD Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTMD Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMD This virtual contains the RETE AC electromagnetic wave data from band D in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:50 1996-03-01 04:59:42 TSS : TSS-1R : RETE : RETE : RTME Ex: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Ey: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Ez: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Bx: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Bz: Input 1 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Ex: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Ey: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Ez: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Bx: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Bz: Input 2 TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTME Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTME This virtual contains the RETE AC electromagnetic wave data from band E in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 4 1996-02-23 06:27:50 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ex: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ey: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ez: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Bx: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Bz: Input 1 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ex: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ey: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Ez: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Bx: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Bz: Input 2 TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Imag Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ex,Ex) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ex,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ex,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ex,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ex,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ey,Ey) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ey,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ey,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ey,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ez,Ez) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ez,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Ez,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Bx,Bx) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Bx,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTMF Real Xcor Spec (Bz,Bz) TSS:TSS-1:RETE:RETE:RTMF This virtual contains the RETE AC electromagnetic wave data from band F in the medium frequency range. The experiment measures the electric field fluctuations along all three principle axes. The x component is measured by means of a monopole/canister system while the y and z components are measured by means of two orthogonal dipoles. Magnetic fluctuations are only along the x and z directions using two search coils. There are two sets of analog input channels, designated 1 and 2, form which the field measurements are made. These should be calibrated independently, that is each should have a unique set of coefficients C1-C3 (defined below). Until there is evidence to the contrary, however, the coefficients for both inputs will be identical The data from sensors 0-9 are converted to physical units through the algorithm: E = 10**{C1[J]*AGC[J]/10} * N * 10**{(C2[J]*atten[J] + C3[J])/10} * 10**{C0/10} where: J denotes the input (1,2) E is in microvolts**2/Hz C0 corrects for the differences of shape of the frequency channels of the digital filter across one AGC band C1 is the coefficient of proportionality for the AGC correction C2 is the coefficient of proportionality for the attenuator C3 corrects for the differences of gain of the analog circuits of the different AGC bands N is the uncompressed telemetry If we denote the two analog inputs as x1 and x2, where x represents Ex, Ey, Ez, Bx, or Bz, then the output for each of the ten steps of the sensor cycle (Ex1,Ex2, Ex1,Ey2, etc) forms a 2x2 cross-spectral matrix. The auto and cross-spectral coefficients are converted to physical units through the algorithm E = 10**{(C1[1]*AGC[1] + C1[2]*AGC2[2])/20} * N * 10**{(C2[1]*atten[1] + C2[2]*atten[2] + C3[1] + C3[2])/20} * 10**{C0/10} The following is a list of tables which are in this vidf TABLE 0: lookup table of center band frequencies in KHz TABLE 1: lookup tables decompressing telemetry giving N TABLE 2: lookup table forming 10**(C0/10) for each freq step TABLE 3: lookup table for cal set 0 forming 10**(C1*AGC/10) for input 1 for sensors 0-4 and 10**(C1*AGC/20) for input 1 for sensors 10-39 TABLE 4: lookup table for cal set 1 giving 10**{(C2*att+C3)/10} for input 1 for sensors 0-4 and 10**{C2*att+C3)/20} for input 1 for sensors 10-39 TABLE 5: lookup table for cal set 3 forming 10**(C1*AGC/10) for input 2 for sensors 5-9 and 10**(C1*AGC/20) for input 2 for sensors 10-39 TABLE 6: lookup table for cal set 4 giving 10**{(C2*att+C3)/10} for input 2 for sensors 5-9 and 10**{C2*att+C3)/20} for input 2 for sensors 10-39 TABLE 7: ascii definitions for cal set 2 TABLE 8: ascii definitions for cal set 5 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Scan all 0 0 kilohertz Sweep 0-4 1,2,3,4 0,3,3,3 microV**2/Hz Sweep 5-9 1,2,5,6 0,3,3,3 microV**2/Hz Sweep 10-39 1,2,3,4,5,6 0,3,3,3,3,3 microV**2/Hz Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 10 1996-02-23 06:27:51 1996-03-01 04:59:43 TSS : TSS-1R : RETE : RETE : RTRLP Pnts Per Swp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Floating Pot TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Plasma Pot (2 Tan) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Plasma Pot (Max 1st Drv) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Plasma Temp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Den (Max 1st Drv) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Den (2 Tan) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP p+ Den TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP IV Fit Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Float Pot Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP p+ Den Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Plasma T Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Den Qual (linear fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Den Qual (log fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Plasma Pot Qual (2 Tan) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Trans Fit Near Vf TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP Trans Fit Below Vp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Above Vp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Near Vp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP p+ Sat Fit Slope (lin fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP p+ Sat Fit Inter (lin fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Slope (log fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Inter (log fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Slope (lin fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : RETE : RETE : RTRLP e- Sat Fit Inter (lin fit) TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. The following is the text that accompanied the data files. The RETE Langmuir Probe data were extracted in ASCII format from the IDFS data files at the SOC, using the ASCII extraction routine which was available to us ( not supported by CAS). At this stage, the calibration of both the LP sweep voltage and the LP current values are still subject to a detailed validation. We have not received yet the updated RETE IDFS documentation which has surely been produced after the modifications of the RETE IDFS which was made in the Nov '95- Dec' 95 timeframe. The latest documentation available to us is dated August 25 1995. A refinement of the LP calibration will also be necessary since it is known that the measured current is somewhat a function of the equivalent LP impedance in the plasma. All the data necessary to calibrate this effect have been acquired pre-flight, but they had not been fully reduced before the flight. Since during the preliminary data analysis phase at the SOC, it proved important to include properly this effect for a proper analysis of the LP I-V curves, a special effort was made to calibrate this effect away in order to obtain reliable plasma parameters. I am now confident that the electron plasma density values are accurate to well within a factor of 2 and that the electron temperature value is accurate to well within a factor of 1.5. The ion plasma density is also probably accurate to a factor of 2 when the probe is located in the ram, but the accuracy is degraded to TBD when we are in the wake. AN IMPORTANT POINT: the preliminary processing of the LP I-V curve assumes that we have "standard" I-V characteristics. The main assumptions made are: i) the plasma is maxwellian; ii) we have only one electron population; iii) only ram ions are considered. In many cases the electron distribution is a two component distribution and this is not taken into consideration yet; more important, when there is some gas release around the satellite there are a lot of thermal, non-ramming ions resulting from the ionisation of the gas. This population is not properly extracted from the analysis. More generally, ion populations resulting from the ionisation in the sheath are not properly extracted by using the standard LP analysis. LP I-V curve analysis method: The method was described in several ESA/ESTEC/SSD internal notes: 1) Analysis method for the RETE Langmuir Probe I-V characteristics, J-P. Lebreton ,18 Feb. 1993 2) Analysis Method of the Langmuir Probe I-V characteristics (Rev. 1) , J.-P. Lebreton, 15 Mar. 1996 The complete analysis method will be thoroughly described in a technical note which will include a description of the analysis of non-standard I-V curves. A more detailed description and the interpretation of the various quality flags and fit coefficients is still subject to current work. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2, 3 volts 4 degrees K 5, 6, 7 cm**-3 8-24 unitless J-P. Lebreton ESA/ESTEC, Solar System Division Postbus 299 2200 AG Noordwijk, The Netherlands e-mail: jlebreto@estec.esa.nl 1 1996-02-25 08:28:08 1996-02-26 01:00:03 TSS : TSS-1R : ROPE : ROPE : RPBB BMSP I TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPBB Meas BMSP V TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPBB Cmd BMSP V TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Num of Peaks TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 1: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 2: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 3: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 1: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 2: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDM Peak 3: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDP Defl TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDP Retard TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDP Retard/Pk 1 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDP Retard/Pk 2 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPDP Retard/Pk 3 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEA e- Sen 3 TSS:TSS-1R:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEA e- Sen 4 TSS:TSS-1R:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEA e- Sen 5 TSS:TSS-1R:ROPE:ROPE:RPEA This virtual consists of data from the three satellite mounted electron SPES sensors. Sensors are mounted at an azimuthal angle of 135 degrees from the science boom and at polar angles of 0, 45 and 85 degrees (sensors 0, 1, and 2 respectively). The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Electron Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEB e- Sen 1 TSS:TSS-1R:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEB e- Sen 2 TSS:TSS-1R:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPEM Dif/Elec TSS : TSS-1 : ROPE : ROPE : RPEM This virtual instrument contains the DIFP electrometer data The following is a list of tables which are in this vidf TABLE 0: lookup table converting telemetry to amps The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 4 1996-02-23 06:33:00 1996-02-28 06:28:52 TSS : TSS-1R : ROPE : ROPE : RPHA FmtCntr/Lo TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA FmtCntr/Hi TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA Cyc/Cntr TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA Cmd/Word TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA DIFP-E/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA DIFP-S/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHA EPROM/Chksm TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB DifV -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB RtdV 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHB ColI 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 1 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 1 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 2 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 2 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 30V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC HVPS 30V I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC PPS1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHC PPS2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES1/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES2/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES3/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES4/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES5/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES1/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES2/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES3/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES4/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHD SPES5/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP 0V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FS +28V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FS +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FS +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FS -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FS 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE FPS T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE HVPS1 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE HVPS2 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE CEP El T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHE MF Cntr TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHF PPS1/+V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHF PPS1/-V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHF PPS2/+V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHF PPS2/-V TSS | TSS-1 | ROPE | ROPE | RPHF This virtual instrument contains the programmable power supply (PPS) voltage monitors. They are stored in vector format. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting scan index value to (eV) TABLE 1: Polynomial coefficients converting telemetry to volts TABLE 2: Gain change corrections in voltage measurement The following are units which can be derived from the tables. TYPE WHICH TABLES OPERS UNIT scan - 0 0 ev swp all 1 2 0 3 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPHG FPS I/Monitor TSS | TSS-1 | ROPE | ROPE | RPHG This virtual instrument contains the floating power supply (FPS) current monitor. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to uamps The following are units which can be derived from the tables. TYPE TABLES OPERS UNIT swp 0 0 microamps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPIA p+ Sen 3 TSS:TSS-1R:ROPE:ROPE:RPIA This virtual consists of data from the satellite mounted ion SPES sensor. The sensors is mounted at an azimuthal angle of 135 degrees from the science boom and at a polar angles of 0 degrees. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Satellite Mounted Ion Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPIB p- Sen 1 TSS:TSS-1R:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPIB p- Sen 2 TSS:TSS-1R:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1996-02-24 08:27:18 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA SPES 1 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA SPES 2 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA SPES 3 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA SPES 4 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA SPES 5 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA HVPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA HVPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA PPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSA PPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB FPS Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB FPS Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB FPS Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS1 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS1 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS1 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS2 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS2 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB PPS2 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB HVU Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB Grid Bias Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB Macro Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB DIFP Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB FPS Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB Tele Test TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSB End Cmd TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Pot:Seek Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Pot:Track Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Pot:Seek/Track Fail TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Pwr Comsump. TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Perf Pwr Consump Chk TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Bad Readings TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Bad FPS/V Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSC Bad BMSP/I Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD RAM I/O Timer1: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD RAM I/O Timer1: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD RAM I/O Timer2: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD RAM I/O Timer2: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD 2K RAM: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD 2K RAM: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD 8K RAM: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : ROPE : ROPE : RPSD 8K RAM: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAA Yaw Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAA Roll Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAA Roll Update Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAA Pitch Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAA Pitch Update Angle TSS:TSS-1:SAHK:SAHK:SHAA This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Yaw Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Yaw Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Roll Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Roll Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Pitch Angle TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAB Scaled Pitch Rate TSS:TSS-1:SAHK:SAHK:SHAB This virtual contains the satellite scaled roll, pitch and yaw data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-2 to degrees and sensors 3-5 to degrees/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees Sweep 3-5 0 0 degrees/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC X Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC Y Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC Z Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC S Gyro Rate TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC ES1 Sun Pres TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAC ES2 Sun Pres TSS:TSS-1:SAHK:SAHK:SHAC This virtual contains the satellite gyro rates and the sun presence monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry of sensors 0-3 to degrees/sec and sensors 4-5 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees/sec Sweep 4-5 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAD Alpha Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAD Beta Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAD Gamma Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAD Skew Angle TSS:TSS-1:SAHK:SAHK:SHAD This virtual contains the satellite gyro angular position data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking the telemetry to radians The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 32 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Coarse Const X Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Coarse Const Y Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Coarse Const Z Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Coarse Const S Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Fine Const X Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Fine Const Y Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Fine Const Z Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Fine Const S Drift TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Ref Hold Ang TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Const Ref Hold Ang TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAE Yaw Rate TSS:TSS-1:SAHK:SAHK:SHAE This virtual contains the satellite yaw, roll and pitch monitors. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-9 radians Sweep 10 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAF Ref Spin Rate TSS:TSS-1:SAHK:SAHK:SHAF This virtual contains the satellite spin rate data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to radians/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAF Cur Ref Spin Rate TSS:TSS-1:SAHK:SAHK:SHAF This virtual contains the satellite spin rate data The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to radians/sec The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 radians/sec G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG Alpha 1/2 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG Alpha 3/4 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG Beta 1/2 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG Beta 3/4 Angle TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG ES1 Chord 1 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG ES1 Chord 2 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG ES2 Chord 1 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHAG ES2 Chord 2 Ang TSS:TSS-1:SAHK:SAHK:SHAG This virtual contains the satellite gyro and angular attitude monitors. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA Flag 3 (Test) TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA TLC Buf 1 Error TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA TLC Buf 2 Error TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA Warmup TmOut TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA TULC TmOut TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA AMSAS Entry Pnt TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA TULC 1st NOGO TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA Scaled Tm To Dock TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA I/O Pl Oper Mode TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA SAS 1st Run TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA SAS InLn2 Closed Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA SAS InLn2 Open Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHA TUCL InLn2 Closed Sent TSS:TSS-1:SAHK:SAHK:SHHA This virtual contains miscellaneous satellite housekeeping monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 4 and 7 to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 3,4,7 0 0 seconds Sweep 0-2,5,6,8-12 0 0 integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHB Onboard Time TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHB Bat1/Bat2 Int Cur TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHB Bat3/Bat4 Int Cur TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHB Sat Ener Consump TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHB P/L Ener Consump TSS:TSS-1:SAHK:SAHK:SHHB This virtual contains the 24 bit satellite battery current and power monitors. The satellite onboard time is also in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds for sensor 1, telemetry to amps/hr for sensors 1 and 2, and telemetry to watts/hr for sensors 3 and 4. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 seconds Sweep 1,2 0 0 amps/hr Sweep 3,4 0 0 watts/hr G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Elapsed Time TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Crew Sleeping Time TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Long TULC Timeout TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Time To Docking TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Time To Dplyment TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHC Time To Retrieval TSS:TSS-1:SAHK:SAHK:SHHC This virtual contains miscellaneous timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to seconds The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 seconds G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD Cmd Mode TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD 1st Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD 2nd Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD 3rd Data Word TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD Updating Proced Run TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD Nshot TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHD Fire Pos/Neg TSS:TSS-1:SAHK:SAHK:SHHD This virtual contains various high time resolution satellite 8 bit monitors There are no VIDF tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHE I/O Pl Sel Valve TSS:TSS-1:SAHK:SAHK:SHHE This virtual contains the low time resolution satellite 3 bit monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor 1 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHE Phase Id # TSS:TSS-1:SAHK:SAHK:SHHE This virtual contains the low time resolution satellite 3 bit monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor 1 The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHF RX Coherent AGC TSS:TSS-1:SAHK:SAHK:SHHF This virtual contains the satellite RX Coherent AGC and loop stress monitors The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry for sensor 0 t0 DbM telemetry for sensor 1 to degrees The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 DbM Sweep all 0 0 degrees G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHHF Loop Stress TSS:TSS-1:SAHK:SAHK:SHHF This virtual contains the satellite RX Coherent AGC and loop stress monitors The following is a list of tables which are in this vidf TABLE 0: lookup tables taking telemetry for sensor 0 t0 DbM telemetry for sensor 1 to degrees The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 DbM Sweep all 0 0 degrees G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 4 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:1 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:2 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:3 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:4 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:5 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:6 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:7 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMA OBDH RSMN:8 RTUP TSS:TSS-1:SAHK:SAHK:SHMA This virtual contains the onboard data handling RSMN monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMB OBDH ASMIN CH T1 TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMB OBDH ASMIN CH T2 TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMB OBDH ASMIN CH T1 RTUP TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMB OBDH ASMIN CH T2 RTUP TSS:TSS-1:SAHK:SAHK:SHMB This virtual contains the satellite onboard data handling ASMN voltage monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 volts-dc G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp St Add TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D1 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D1 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D1 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D1 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D2 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D2 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D2 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D2 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC DH UP MDmp D3 TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp St Add TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D1 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(0-15) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(16-31) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(32-47) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D2 b(48-63) TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC AMCS UP MDmp D3 TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Cntr TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf1 Msg# TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf2 Msg# TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf1 Exp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf2 Exp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf1 Comp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC TLC Buf2 Comp Chksm TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC Fmt Cntr TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMC Fmt Num TSS:TSS-1:SAHK:SAHK:SHMC This virtual contains the satellite memory dump and TLC data. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all hex/integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH PROM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH G-RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH FGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH BGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH Subr Err TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH Stck Ovrflow TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD OBDH Self Chk TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS Up Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS PROM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS G-RAM Status TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS FGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS BGP Ovrrun TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS Subr Err TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS Stck Ovrflow TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS Self Chk TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD AMCS GR Acc Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD BUS Arbtr Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD RTUS Arbtr Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD GR Access Fail TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD > 2 Blks TLCS TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD CTU-RTUS Link TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHMD CTU-RTUP Link TSS:TSS-1:SAHK:SAHK:SHMD This virtual contains the satellite onboard data handling system and AMCS status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii definitions for sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHME OBDH FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHME OBDH BGF # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHME AMCS FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHME AMCS FGP # Ovrrun TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHME AMCS Oper. Mode TSS:TSS-1:SAHK:SAHK:SHME This virtual contains some of the satellite onboard data handling and AMCS monitors There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat1/Bat2 I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat4/Bat4 I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Main Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA OBDH Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA TT&C Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA PPDA Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA AMCS Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA PM Heater Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA D&J Heater Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA I/O Pl Sec Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA APS Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Yaw Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Rel/L Valve Bus I TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat 2 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat 4 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat1/Bat2 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Bat3/Bat4 V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA Main Bus V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA TX Reg V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA RX Reg V TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHPA TX RF Output Pwr TSS:TSS-1:SAHK:SAHK:SHPA This virtual contains some of the satellite bus current and voltage monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps for sensors 0-12, and to voltage for sensors 13-19. There is a lookup table taking telemetry from sen 20 to DbM. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-12 0 0 amps Sweep 13-18 0 0 voltage Sweep 20 0 0 DbM G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Status TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA X Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Y Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Z Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA S Gyro Warmup TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA X Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Y Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Z Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA S Gyro Chkout TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Pkg 1 X Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Pkg 1 Z Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Pkg 2 Y Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Gyro Pkg 2 S Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA X Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Y Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Z Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA S Gyro Cmd TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Earth Sen TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Sun Sen TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA EL/1 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA EL/2 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/1 Served TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/2 Served TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/1 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/2 OK TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/1 Hd Flg TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/2 Hd Flg TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/1 Int Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA ES/2 Int Temp TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Yaw 1 Cmd Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Yaw 2 Cmd Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Yaw 1 Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSA Yaw 2 Flag TSS:TSS-1:SAHK:SAHK:SHSA This virtual contains the low temporal resolution satellite gyro monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB X Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Y Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Z Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB S Gyro Convtr TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB X Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Y Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Z Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB S Gyro Heating TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB X Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Y Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB Z Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSB S Gyro Wheel TSS:TSS-1:SAHK:SAHK:SHSB This virtual contains the satellite gyro converter, heating and wheel monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSC FDS3/FDS4 Status TSS:TSS-1:SAHK:SAHK:SHSC This virtual contains the low time resloution satellite FDS3/FDS4 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSC FDS3/FDS4 Sun TSS:TSS-1:SAHK:SAHK:SHSC This virtual contains the low time resloution satellite FDS3/FDS4 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD GYMODE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD GYOPS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD GYCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD GYWU Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD GYRO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ACQGYR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ATTITUDE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PASSIVE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SPIN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD HOLD Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD RETR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ONST Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD DEPL Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD VRPH1 Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD VRPH2 Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD RTUPQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD RTUSQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD TIMSLEEP Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD TIMCOUNT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD Start Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD IOFIRE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD CA Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD TFGEN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ICOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD LM Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SRM Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD RERE Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ROMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PRPO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD TTOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SAS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD TULC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PMTC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PEPC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD PEPC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD DPPH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SWITCH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD AQTEST Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD CONTROL Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD AFTGEN Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ACA Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD AICOUT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SVISOR Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD AMSAS Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD UPDAT Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD AROMQ Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD YAWTH Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD APCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ESCO Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD SSTC Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSD ESUP Prgm Stat TSS:TSS-1:SAHK:SAHK:SHSD This virtual contains the satellite program status flags. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 01: ROPE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 09: ROPE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 02: ROPE Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 03: TEMAG Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 04: TEMAG Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 07: RETE Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 08: RETE Htr Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 06: Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE P/L 12: Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE GPS Pwr TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE Main Iso Valve TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE In Line 1 Valve TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE RX Lock TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE Temp 3 Warning TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSE Temp 4 Warning TSS:TSS-1:SAHK:SAHK:SHSE This virtual contains some of the satellite medium temporal status monitors. The experiment power line status' are contained here. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Bat1/Bat2 Cur Sign TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Bat3/Bat4 Cur Sign TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Temp1 Warning TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Temp2 Warning TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF InPl Rear Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF InPl Front Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF OutPl Right Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF OutPl Left Valve TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF ES1 Pwr TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF ES1 Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF ES2 Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Ranging Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Squelch Status TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF Frame Valid TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSF ASW Found TSS:TSS-1:SAHK:SAHK:SHSF This virtual contains the medium time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Test Bit Sign TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG P/L Energy Consump TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Uplink Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Valve1 NOGO TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Valve2 NOGO TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Pwr Off Cmd Sent TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Pwr Drop Occur TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG APS Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Crit Fn Rly Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg1 Squelch TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg1 RX Coher AGC TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg1 Lock Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Updating Enabled TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG APS Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Reg Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Tank Pressure TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg5 PM Sec1/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg5 PM Sec2/T2 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg5 PM Sec3/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg6 PM Sec1/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg6 PM Sec2/T2 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Flg6 PM Sec3/T1 TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat1 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat2 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat3 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat4 Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat Temp Status TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG APS Pres Reg Temp TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSG Bat Verification TSS:TSS-1:SAHK:SAHK:SHSG This virtual contains miscellaneous low temporal resolution satellite monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH InLine 2 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH I/O OfPl Iso Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH Yaw 1 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH Yaw 2 Valve TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH ES1 Pwr TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSH TX Pwr TSS:TSS-1:SAHK:SAHK:SHSH This virtual contains the high time resolution satellite status monitors. Some of the valve status' are found here The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for sensor Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI Bat1/Bat2 Status TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI Bat3/Bat4 Status TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI TT&C Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI PPDA Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI AMCS Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI APS Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI PM Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI I/O Pl Sec Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI Yaw Sec Pwr TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSI TX Pwr Enable TSS:TSS-1:SAHK:SAHK:SHSI This virtual contains the several of the satellite power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Alpha 1/2 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Alpha 3/4 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Beta 1/2 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Beta 3/4 Selected TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Alpha 1/2 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Alpha 3/4 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Beta 1/2 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ Beta 3/4 Data Valid TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ FDS1/FDS2 Status TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSJ FDS1/FDS2 Sun TSS:TSS-1:SAHK:SAHK:SHSJ This virtual contains the satellite alpha, beta and FDS1/FDS2 status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK Yaw/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK Yaw/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK InPl/Rear TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK InPl/Frnt TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK OutPl/Right TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK OutPl/Left TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK InLn/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHSK InLn/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA Gyro Pkg 1 Temp X TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA Gyro Pkg 1 Temp Z TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA Gyro Pkg 2 Temp Y TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA Gyro Pkg 1 Temp S TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA ES1 Int Temp TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTA ES2 Int Temp TSS:TSS-1:SAHK:SAHK:SHTA This virtual contains the satellite Gyro and earth sensor temperature monitors The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec1 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec1 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec2 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec2 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec3 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec3 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec4 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Sec4 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec1 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec1 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec2 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec2 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec3 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec3 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec4 T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB PM Skin Sec4 T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T3 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T4 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T5 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T6 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T7 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T8 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T9 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T10 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T11 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T12 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T13 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T14 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T15 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Env T16 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T1 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T2 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T3 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T4 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T5 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T6 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T7 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTB SM Skin T8 TSS:TSS-1:SAHK:SAHK:SHTB This virtual contains the satellite temperature monitors. Note the following modification per instructions from ALENIA to correct for faulty readings from sensor 12, the telemetry value is corrected to TM = 2 * OLDTM - 190 This is accomplished in the first VIDF table The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients modifying sensor 12's TM TABLE 1: polynomial coefficients taking telemetry to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 12 0,1 0,0 degrees C Sweep 0-11,13-39 1 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Tank Pres TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Regulated Pres TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Battery 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Battery 2 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Battery 3 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC Battery 4 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS Pres Reg Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS Tank Sur Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS Out Tank Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS ATH 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS ATH 3 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS InLine 1 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS InLine 2 Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS InPl Rear Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS InPl Frnt Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS OutPl Valve Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS I/OutPl Iso Valve T TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC APS Yaw 1/2 Valve Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC TX Final Stge Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SAHK : SAHK : SHTC RX Temp TSS:TSS-1:SAHK:SAHK:SHTC This virtual contains the satellite some of the satellite pressure and temperature monitors. Most of the battery and inline monitors are in this virtual The following is a list of tables which are in this vidf TABLE 0: A mixture of polynomial coefficients and look up tables taking telemetry to degrees C or pascals (sens 0 & 1) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0-1 0 pascals Sweep all 2-19 0 degrees C G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAC SLA/X TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAC SLA/Y TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAC SLA/Z TSS:TSS-1:SCORE:SCORE:SCAC This virtual contains the low resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAF SLA/X TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAF SLA/Y TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCAF SLA/Z TSS:TSS-1:SCORE:SCORE:SCAF This virtual contains the high resolution satellite vector accelerometer measurements. The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to milli-g The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 0 milli-g Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMA SLA:Coarse T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMA SLA:Fine T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMA SLA:Filter T TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMA SLA:DC/DC Reg V TSS:TSS-1:SCORE:SCORE:SCMA This virtual contains the SLA temperature and voltage housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensors 0-2 to degrees C and sensor 3 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMB SA:Temp TSS:TSS-1:SCORE:SCORE:SCMB This virtual contains the SA temperature and overtemperature housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensor 0 to degrees C and sensor 1 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 degrees C Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMB SA:OverTemp TSS:TSS-1:SCORE:SCORE:SCMB This virtual contains the SA temperature and overtemperature housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry for sensor 0 to degrees C and sensor 1 to volts-dc The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 degrees C Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMC SV/Ovflow TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMC SV/Achk/S TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMC SV/AChk TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCMC Tether/I TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSA P/L Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSA H/K Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSA P/L 05 SA Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSA P/L 10 SLA Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSA P/L 11 HTR Pwr TSS:TSS-1:SCORE:SCORE:SCSA This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSB SLA Oper TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSB SA Pwr Chk TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SCORE : SCORE : SCSB SA Autochk Cmd TSS:TSS-1:SCORE:SCORE:SCSB This virtual consists of the low time resolution event flags for the SCORE experiment. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : SETS : SETS : STAA Bx TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STAA By TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STAA Bz TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS aspect magnetometer data. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCA Cur Den (Peak) TSS:TSS-1:SETS:SETS:STCA This virtual contains the peak monitors in the SETS current and charge probe The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCA Charge Den (Peak) TSS:TSS-1:SETS:SETS:STCA This virtual contains the peak monitors in the SETS current and charge probe The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCB Cur Den (Dir) TSS:TSS-1:SETS:SETS:STCB This virtual contains the SETS direct current and charge probe monitors. The data is transmitted as separate 8 and 4 bit values and is combined within this virtual to a single 12 bit data word. The 4 bits is the lowest 4 bits. The telemetry scaling to physical units was given only for the 8 bit data, of the form Value = A + Tele * B To compensate for adding the bottom 4 bits, the scaling factor B has been divided by 16 in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCB Charge Den (Dir) TSS:TSS-1:SETS:SETS:STCB This virtual contains the SETS direct current and charge probe monitors. The data is transmitted as separate 8 and 4 bit values and is combined within this virtual to a single 12 bit data word. The 4 bits is the lowest 4 bits. The telemetry scaling to physical units was given only for the 8 bit data, of the form Value = A + Tele * B To compensate for adding the bottom 4 bits, the scaling factor B has been divided by 16 in this virtual. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients telemetry for sensor 0 to milliamps/m and telemetry for sensor 1 to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 milliamps/m Sweep 0 0 0 volds-dc Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Cur Filter In TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Cur Calib TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Cur Enable TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Q Reset TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Q Enable TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Relay TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCC CCP Pwr TSS:TSS-1:SETS:SETS:STCC This virtual contains the SETS CCP status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP Probe Elec T TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP +15V Bus V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP -15V Bus V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD Q Probe Off V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD Cur Probe Off V TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD CCP Current TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STCD Time CCP Rlys On TSS:TSS-1:SETS:SETS:STCD This virtual contains the SETS CCP general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-2 to degrees C, telemetry from sensors 3-6 to volts, and telemetry from sensor 7 to amps. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-2 0 0 degrees C Sweep 3-6 0 0 volts-dc Sweep 7 0 0 amps Sweep 8 0 0 seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA DEP MN Frm Cur Cnt TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA Fault Code1 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA Fault Code2 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA FLT1 Running Tot TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA FLT2 Running Tot TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA Oper Mode TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA Oper Cycle TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA Oper Step TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA DEP Msg Stat Wd TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA DEP I TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA DEP T1 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDA DEP T2 TSS:TSS-1:SETS:SETS:STDA This virtual contains the SETS DEP housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 9 to amps, and from sensors 10-11 to degrees C. TABLE 1: Ascii State definitions of sensor states for sensors 1-2, 5-6, and 8 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 9 0 0 amps Sweep 10-11 0 0 volts-dc Sweep 3-4,6 - - counts Sweep 0-2,5-6,7-8 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDB OCI Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDB OMI Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDB Step Time To Go TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDB CPU Tm at Mn Frm 0 Req TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDB TM Pg Chksum TSS:TSS-1:SETS:SETS:STDB This virtual contains the DEP operation timing monitors. Note: Sensor 4, the Telemetry Page Checksum, is saved in little-endian format, just as it is in the telemetry page, as that is its significant form. There are no tables associated with this virtual. The data is stored in floating format, already in physical units The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep 0-1 seconds Sweep 3 milliseconds Sweep 4 integer/hex Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDC CPU On Time TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDC Multibus Tm Bytes 1-3 TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDC Multibus Tm Bytes 4-6 TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDC Mn Frm Cnt 0 Time TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STDC GMT TSS:TSS-1:SETS:SETS:STDC This virtual contains SETS DEP timing monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 1 to seconds, and from sensor 2 to milliseconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,3 - - milliseconds Sweep 1 0 0 seconds Sweep 2 0 0 microseconds Sweep 4 - - seconds Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG Current TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 Focus Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 Anode Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 HV Conv Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 Focus Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 Anode Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 HV Conv Cur TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 Charge Out TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 Charge Out TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 Pre-reg +20V TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 HVPS TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 Pre-reg +20V TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 HVPS TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun1 Fila Conv T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun2 Fila Conv T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Gun Elec T TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG +15V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG +5V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG -15V Bus TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG # Pulses TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG Pulse Off Tm TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG Pulse On Tm TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA Time FPEG Fila On TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFA FPEG Cmd Cntr TSS:TSS-1:SETS:SETS:STFA This virtual contains the SETS FPEG general housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-6 to amps, telemetry from sensors 7-8 to coulombs, telemetry from sensors 9-12 and 16-18 to volts, telemetry from sensors 13-15 to degrees C, and telemetry from sensors 20-21 to seconds. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-6 0 0 amps Sweep 7,8 0 0 coulombs Sweep 9-12,16-18 0 0 volts-dc Sweep 13-15 0 0 degrees C Sweep 19 0 0 integer Sweep 20-21 0 0 seconds Sweep 22 - - seconds Sweep 23 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Pwr TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB EGA Sync1 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB EGA Sync2 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Enable Pulses Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Enable Off Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Enable On Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Fila Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Fila Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Fila On Tmr Set TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Fila On Disc TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG HV Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG HV Enable Var TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG HV Arm TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG HV On TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Run Bar Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Gun1 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Gun2 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Run TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Stop TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Stret Gun Pulse TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Go Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Send Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Ready Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Cur Limit TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB FPEG Squel Enable TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STFB Gun Sw Pulse Mon TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMA Heater Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMA SRPA Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMA SPIB Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMA AMAG Pwr TSS:TSS-1:SETS:SETS:STMA This virtual contains the SETS power status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB AMAG Current TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB SPIB Current TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB SPIB Voltage TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB SPIB T1 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB SPIB T2 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STMB SPIB T3 TSS:TSS-1:SETS:SETS:STMB This virtual contains the SETS AMAG and SPIB housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, telemetry from sensors 2 to volts, and and telemetry from sensors 3-5 to degrees C. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2 0 0 volts-dc Sweep 3-5 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSA LangP Swping TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSA LangP Flybk TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSA LangP Srch Mode TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSA LangP Short Swp TSS:TSS-1:SETS:SETS:STSA This virtual contains the SETS Langmuir probe data. The Langmuir Probe is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. The sweep charaacteristics of the Langmuir probe are determined by the SRPA voltage steps. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in minor frames 0, 6, 12, and 18 within the SETS telemetry page. The Langmuir Probe sweep voltage is only sampled once per second; its sweep value is sampled during minor frame 23 and returned in that frame. Because the Langmuir Probe sweeps are synchronous with the SRPA instrument, and because the SRPA sweep voltages are returned at a higher rate, they are used to determine the Langmuir sweep type and hence the selected sensor. The Langmuir probe sweep voltage is returned within the data record in cal set 0, but is not explicitly used to either determine the sweep characteristics or to form the sweep voltage steps. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 LP data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Hi Sens SRPA Swping TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Hi Sens SRPA Flybk TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Hi Sens SRPA Srch Mode TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Hi Sens SRPA Short Swp TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Low Sens SRPA Swping TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Low Sens SRPA Flybk TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Low Sens SRPA Srch Mode TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSB Low Sens SRPA Short Swp TSS:TSS-1:SETS:SETS:STSB This virtual contains the SETS Spherical Retarding Potential Analyzer (SRPA). The SRPA is a free running instrument whose sweep length is not longer than 30 seconds, but may be any length up to this value. There are 4 sweep voltage values returned per second for the SRPA instrument. These are associated with the data in in minor frames 0, 6, 12, and 18 within the SETS telemetry page. These voltages are returned in cal set 0. The beginning and ending of any sweep as well as the type of sweep (sensor) is determined by an algorithm using the returned SRPA sweep voltages. The algorithm is basically the following. Using the previous (P) and next (N) voltage step, the 6 LP values associated with the current (C) voltage step are within a normal sweep if (C-P) > -1 and (N-C) > -1 are within a flyback if (C-P) < -1 and (N-C) < -1 and are within a search mode sweep if (C-P) > 3 and (N-C) > 3. If none of these conditions hold then the data is in the same mode as determined for the last set of 6 SRPA data values. A sweep ends when the transition from either normal or search mode sweep to flyback is observed and a sweep begins when the transition from flyback to either normal or search mode sweep occurs. A short sweep is defined as any normal sweep which lasts less than 5 seconds. The samp_index array in the header record is formed by a linear fit to the sweep voltages acquired during a sweep acquisition. The fit coefficients are returned in calibration sets 1-4. These are used to estimate the voltage at each sweep step. The voltage is derived by: V[i] = slope * scan_index[i] + offset Although this is a vector virtual instrument, it is not handled or assembled as most vector virtual instruments. The sweep length of the virtual instrument is variable and may extend over several SETS major frames. To avoid selecting a data array size which is too large to just to ensure that the largest sweep will fit into it, and so possibly waste needless storage space, the sweep is broken up into 6-step components. Each sensor set defines a maximum of 6 steps of a sweep. A sweep is defined as all of the data taken between two voltage flyback, or two occurrances of sensor 1. The following is a list of tables which are in this vidf TABLE 0: look up table taking sensor telemetry to Db TABLE 1: polynomial coefficients taking cal set 1 to the most significant part of slope; used in getting scan voltage TABLE 2: polynomial coefficients taking cal set 2 to the least significant part of slope; used in getting scan voltage TABLE 3: lookup table taking scan_index to scan_index. This is a trivial tables used in computing the scan voltage TABLE 4: polynomial coefficients taking cal set 3 to the most significant part of offset; used in getting scan V TABLE 5: polynomial coefficients taking cal set 4 to the least significant part of offset; used in getting the scan V TABLE 6: polynomial coefficients taking cal set 0 to volts TABLE 7: ascii definition of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN/CAL TABLES OPERS UNIT Sweep S0 0 0 Db Scan - 1,2,3,4 5 0 1 * 1 1 volts Cal C0 6 0 volts Slope C1,C2 1,2 0,1 - Offset C4,C5 4,5 0,1 - Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 16 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC Htr Cur TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC SRPA Cur TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC +6V SRPA Bus V TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC -6V SRPA Bus V TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC 10.5 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC 8.5 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC LP 3.2 kHz Ampl TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC Analyzer Elec T TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STSC Preamp T TSS:TSS-1:SETS:SETS:STSC This virtual contains the SETS SRPA housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-1 to amps, from sensors 2-3 to volts, from sensors 4-6 to dB and sensors 7-8 to degrees C The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-1 0 0 amps Sweep 2-3 0 0 volts Sweep 4-6 0 0 dB Sweep 7-8 0 0 degrees C Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTA Tether I TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS tether current monitor. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps TABLE 1: polynomial coefficients taking telemetry to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 0 1 0 milliamps Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTB Tether V TSS:TSS-1:SETS:SETS:STTB The telemetry for STTB is returned as a 16 bit voltage followed by a set of 7 16 bit voltages or 14 8 bit voltages. In latter case, the telemetry is obtained by shifting the measured 16 bit voltages some number of bits to the right and masking off all but 8 bits. In this virtual instrument all 8 bit data has been shifted back to the left the number of bit indicated in the shift status byte (status byte 1). The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients converting telemetry to volts TABLE 1: ASCII status definitions The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA NUM TABLES OPERS UNIT Sensor 0 0 0 volts Brian Gilchrist Unversity of Michigan 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Current TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM +15V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM +5V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM -15V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM +28V TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Base Plate T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Pwr Sply T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Load RisA T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Load RisB T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Load RisC T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM PROT Cap T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Elec T TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Pres A TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Pres B TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM Lst Cmd Sent TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTC TCVM TVM AC Gain Rlys TSS:TSS-1:SETS:SETS:STTC This virtual contains the SETS TCVM monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0 to amps, from sensors 1-4 to volts, from sensors 5-11 to degrees C and from sensors 12-13 to psi TABLE 1: ascii values for states of sensor 15 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 1-4 0 0 volts Sweep 5-11 0 0 degrees C Sweep 12-13 0 0 psi Sweep 14-15 - - integer Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Pwr TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/CAL A/C TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TVM/AC/FC TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TCM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TCM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM TCM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Mux Add B0 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Mux Add B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Mux Add B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Mux Add B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Hskp Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/Gain/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/Gain/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/LPFR/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/LPFR/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/LPFR/ B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMS/Relay TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMS/DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM CMS/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Shunt Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Shunt DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Shunt Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM 2.5 Mohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM 250 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM 25 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM HV Prot TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD TCVM Mech Mode Sw TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SETS : SETS : STTD Prot Cap En Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-22 11:09:42 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod EL7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Ch7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig1 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig2 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig3 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig4 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig5 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig6 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPBA Space Beam Mod Sig7 TSS:TSS-1:SPREE:SPREE:SPBA This virtual contains the SPREE space beam data monitors. The beam data returned in the TSS realtime telemetry is the seven most significant signal levels processed within a data block. These are indicated within the sensors as #1 through #7. Those measurements associated with #1 are associated with the most significant signal level and those associated with #7 are associated with the least significant signal level returned. The following is a list of tables which are in this vidf TABLE 0: lookup tables taking sensors 0-13 to integer values and polynomial coefficients taking telemetry from sensors 14-20 to confidence. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-13 0 0 integer Sweep 14-20 0 0 confidence Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z0 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z1 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z2 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z3 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z4 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z5 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z6 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z7 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z8 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEA Electrons/A Z9 TSS:TSS-1:SPREE:SPREE:SPEA This virtual contains the SPREE peak zone selected electron spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z0 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z1 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z2 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z3 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z4 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z5 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z6 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z7 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z8 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEB Electrons/B Z9 TSS:TSS-1:SPREE:SPREE:SPEB This virtual contains the SPREE peak zone selected electron spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest negative potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z0 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z1 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z2 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z3 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z4 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z5 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z6 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z7 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z8 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPEC Electrons/A Z9 TSS:TSS-1:SPREE:SPREE:SPEC This virtual contains the SPREE azimuthally summed electron spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z0 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z1 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z2 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z3 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z4 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z5 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z6 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z7 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z8 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPED Electrons/B Z9 TSS:TSS-1:SPREE:SPREE:SPED This virtual contains the SPREE azimuthally summed electron spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (time). Consequently, because the data are returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:55 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFA e- Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPFA This virtual contains the electron high frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-02-28 11:39:40 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPFB e- Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPFB This virtual contains the electron high frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to MHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 megahertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:03 1996-02-28 11:39:44 TSS : TSS-1R : SPREE : SPREE : SPHA DPU Base Plate T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA DPU Pwr Supply T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA DPU FDR1 Casing T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA DPU FDR2 Casing T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA HV A Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA HV B Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA MCP A Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA MCP B Temp TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA RTMD A Motor T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA RTMD B Motor T TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA MCP A V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA MCP B V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA +5V Line V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA +12V Line V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA Dif Plate A V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHA Dif Plate B V TSS:TSS-1:SPREE:SPREE:SPHA This virtual contains the SPREE subcommutated housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-9 to degrees C, and from sensors 10-15 to volts. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-9 0 0 degrees C Sweep 10-15 0 0 volts-dc Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 8 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR1 Tape Xsport T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR1 Casing T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR1 Pressure TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR1 Rd/Wr Err Cnt TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR2 Tape Xsport T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR2 Casing T TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR2 Pressure TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHB FDR2 Rd/Wr Err Cnt TSS:TSS-1:SPREE:SPREE:SPHB This virtual contains some of the SPREE FDR housekeeping monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensor 0-3 to degrees C, and from sensors 4-5 to psi. The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-3 0 0 degrees C Sweep 4-5 0 0 psi Sweep 6-7 0 0 integer Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHC FDR1 Tape Cntr TSS:TSS-1:SPREE:SPREE:SPHC This virtual contains the SPREE tape counter monitors. There are no tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHC FDR2 Tape Cntr TSS:TSS-1:SPREE:SPREE:SPHC This virtual contains the SPREE tape counter monitors. There are no tables associated with this virtual instrument. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHD Space Frm Cnt TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHD Space Frm Size TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHD Space Rot Num TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHD Energy Swp Num TSS:TSS-1:SPREE:SPREE:SPHD This virtual contains the SPREE space counter data. The following is a list of tables which are in this vidf TABLE 0: lokup table taking telemetry from sensor 1 to bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0,2,3 - - integer Sweep 1 0 0 bytes Dr Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPHE Uplink Cmd Echo TSS:TSS-1:SPREE:SPREE:SPHE This virtual contains the SPREE uplink command echo. There are no tables associated with this virtual. The units associated with the sensors are defined below DATA TYPE SEN UNITS Sweep all integer/hex Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIA SumIons/A TSS:TSS-1:SPREE:SPREE:SPIA This virtual contains the SPREE summed ion spectrum from ESA A. This particular summed spectrum contains the particle counts divided by 8 to avoid overflow and then summed over all 10 elevation angles (SPREE zones 0-9). Summation of the zones occurs before the division by eight. The division is done regardless of the energy sweep rate. This summed spectrum then contains the particle count at each of the 32 energy levels, summed over zone. If the instrument is in the 8 energy sweeps/sec mode, the summed spectra provided in this telemetry block will be from the energy sweep matching the highest potential determination. If the potential value is 0 or exactly the same for all 8 energy sweeps, the downlinked summed spectrum in the first of the 8. If in the 1 energy sweep/sec mode, these data correspond to the potential information by default. This portion of the telemetry is intended to provide the closest correspondence to the potential determination, specifically for crew use on the PGSE display. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIB SumIons/B TSS:TSS-1:SPREE:SPREE:SPIB This virtual contains the SPREE summed ion spectrum from ESA B. This particular summed spectrum contains the particle counts divided by 8 to avoid overflow and then summed over all 10 elevation angles (SPREE zones 0-9). Summation of the zones occurs before the division by eight. The division is done regardless of the energy sweep rate. This summed spectrum then contains the particle count at each of the 32 energy levels, summed over zone. If the instrument is in the 8 energy sweeps/sec mode, the summed spectra provided in this telemetry block will be from the energy sweep matching the highest potential determination. If the potential value is 0 or exactly the same for all 8 energy sweeps, the downlinked summed spectrum in the first of the 8. If in the 1 energy sweep/sec mode, these data correspond to the potential information by default. This portion of the telemetry is intended to provide the closest correspondence to the potential determination, specifically for crew use on the PGSE display. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z0 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z1 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z2 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z3 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z4 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z5 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z6 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z7 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z8 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIC Ions/A Z9 TSS:TSS-1:SPREE:SPREE:SPIC This virtual contains the SPREE peak zone selected ion spectrum from ESA A. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA B makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA A zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z0 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z1 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z2 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z3 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z4 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z5 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z6 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z7 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z8 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPID Ions/B Z9 TSS:TSS-1:SPREE:SPREE:SPID This virtual contains the SPREE peak zone selected ion spectrum from ESA B. The spectrum is the complete energy spectrum from the zone corresponding to the highest negative potential determination. That determination is made either by ESA A or ESA B. For example, if ESA A makes the potential determination in zone 4, the spectra that are downlinked as the peak-zone-selected come from ESA B zone 4. If in the 8 energy sweeps/sec mode, the spectrum corresponds to the highest potential found in the 8 sweeps. These data are not summed nor are they divided by 8 to prevent overflow. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Capt. Marilyn R. Oberhardt GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z0 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z1 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z2 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z3 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z4 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z5 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z6 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z7 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z8 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIE Ions/A Z9 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA A. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z0 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z1 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z2 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z3 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z4 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z5 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z6 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z7 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z8 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPIF Ions/B Z9 TSS:TSS-1:SPREE:SPREE:SPIE This virtual contains the SPREE azimuthally summed ion spectrum from ESA B. The summation of the data occurs over an azimuth/cycle (i.e. time). Consequently, because the data is returned each second, if the energy sweep rate is 1/sec, this is not really a summation; each measurement will contain the counts (divided by 8 to prevent overflow) in that particular zone at that given instant in time in that energy step. If in the 8 sweep/sec mode, each of the 8 particle counts in a given zone in a given energy step is divided by 8 and then the 8 particle counts for that given zone and energy step are summed. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLA p+ Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPLA This virtual contains the ion low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- AutoCor A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Sig A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- ACor Neu A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z0 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z1 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z2 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z3 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z4 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z5 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z6 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z7 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z8 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLB e- Radar Ret A-Z9 TSS:TSS-1:SPREE:SPREE:SPLB This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:57 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLC p+ Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPLC This virtual contains the ion low-frequency auto-corellation spectra taken from ESA B. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:19:59 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- AutoCor B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Sig B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- ACor Neu B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z0 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z1 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z2 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z3 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z4 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z5 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z6 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z7 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z8 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPLD e- Radar Ret B-Z9 TSS:TSS-1:SPREE:SPREE:SPLD This virtual contains the electron low-frequency auto-corellation spectra taken from ESA A. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: Polynomial coefficients taking the telemetry of sensors 0-9 to kHz and of sensors 10-19 to confidence TABLE 2: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA SENSORS TABLES OPERS UNIT Scan all 0 0 eV Sen 0-9 0 0 kilohertz Sen 10-19 0 0 confidence Sen 20-39 - - integer Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 2 1996-02-23 01:20:01 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPMF Bx TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPMF By TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPMF Bz TSS:TSS-1:SPREE:SPREE:SPMF This virtual contains aspect magnetometer data which is obtained from the SETS magnetometer . The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to nT TABLE 1: polynomial coefficients taking telemetry to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 nanotesla Sweep 0 1 0 gauss Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Orb Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Conf Fac TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Head Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Zone Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Ch Above Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Peak Channel TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPOP Ch Below Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 0 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 1 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 2 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 3 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 4 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 5 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 6 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 7 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 8 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 9 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 10 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Low Freq MMU 11 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b0 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b1 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b2 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b3 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b4 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b5 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b6 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b7 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b8 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b9 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b10 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b11 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b12 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b13 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b14 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSA Space Proc Flow Mon b15 TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the SPREE SPACE status and flow monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSB HV Swp Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB HV Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB Spectra Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB Time Tag Cmd TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB RTMD A Sense TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB RTMD B Sense TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB FDR1 Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSB FDR2 Status TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DPU and FDR sense key status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:58 1996-03-01 11:01:40 TSS : TSS-1R : SPREE : SPREE : SPSC FDR1 Filemark TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR1 Begin or EOT TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR1 CTS TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR1 Pwr Fail/Rec TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR1 Sense Key TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR2 Filemark TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR2 Begin or EOT TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR2 CTS TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR2 Pwr Fail/Rec TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSC FDR2 Sense Key TSS:TSS-1:SPREE:SPREE:SPSC This virtual contains the SPREE FDR tape status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : SPREE : SPREE : SPSD DCORE/SETS Gun Stat TSS:TSS-1:SPREE:SPREE:SPSA This virtual contains the DCORE and SETS gun status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions of sensor states Units are simply instrument states. There are no alternate units Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 1 1996-02-23 01:19:53 1996-03-01 11:01:39 TSS : TSS-1R : TEMAG : TEMAG : TMHA Out/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA In/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA Ele/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA -8V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA +12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA -12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA +5V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHA Spare TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHB TeleCmd Echo TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMHB Chksum TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMI In/Bx TSS:TSS-1R:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMI In/By TSS:TSS-1R:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMI In/Bz TSS:TSS-1R:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:00:29 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMO Out/Bx TSS:TSS-1R:TEMAG:TEMAG:TMMO This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 80 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMO Out/By TSS:TSS-1R:TEMAG:TEMAG:TMMO This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 80 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMMO Out/Bz TSS:TSS-1R:TEMAG:TEMAG:TMMO This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 80 cm from the satellite. The coordinate system used by the magnetometer has -X along the satellite boom, +Z in the direction of the tether, and +Y completes a right-handed set. Note that in the satellite body coordinate system, +Z is the direction away from the tether The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in satellite coordinate system TABLE 1: Polynomial coefficients taking sensor data to gauss with (XYZ) in satellite coordinate system TABLE 2: Polynomial coefficients taking sensor data to nanotesla with (XYZ) in TEMAG coordinate system TABLE 3: Polynomial coefficients taking sensor data to gauss with (XYZ) in TEMAG coordinate system TABLE 4: Ascii definitions of status byte The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla (inst coor sys) Sensor 1 0 gauss (inst coor sys) Sensor 2 0 nanotesla (sat coor sys) Sensor 3 0 gauss (sat coor sys) 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1R : TEMAG : TEMAG : TMTA Tether Cur. TSS:TSS-1:TEMAG:TEMAG:TMTA This virtual contains the tether current data obtained from the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor all 0,1 0,0 mamps 4/23/97 - TEMAG time_off values have been set to -16384 msec to correct for a timming error found in the data records. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Tether Current Obtained from the Satellite Ampmeter 8 1996-02-23 06:00:30 1996-03-01 05:00:13 TSS : TSS-1Ro : CAS : CAS : CSCA Shuttle Lat TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Shuttle Long TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Pitch (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Yaw (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Roll (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Pitch Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Yaw Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Roll Rate (LV,LH) TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Sat Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Sat Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Ram Azimuth TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Ram Co-elev TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCA Orbit # TSS | TSS-1 | CAS | CAS | CSCA This virtual instrument contains data which was computed from values returned within the shuttle CAS data stream. The data is stored as floating point values and are already int the base units shown in the following table SENSOR UNITS | SENSOR UNITS | SENSOR UNITS ----------------------------------------------------------------- 0 degrees | 1 degrees | 2 degrees 3 degrees | 4 degrees | 5 degrees/sec 6 degrees/sec | 7 degrees/sec | 8 degrees 9 degrees | 10 degrees | 11 degrees 12 integer | | Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCB FES Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCB Water Dump Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : CAS : CAS : CSCB Thruster Status TSS:TSS-1:CAS:CAS:CSCB This virtual contains computed acnillary status monitors. Thses are not returned in the telemetry but are built from returned values. monitors. The sensors were constructed according to the folloing algorithms: Sensor 0: Is 0 unless one of the sensors 11-14 in CSSA is one and the averages of sensors 12 and 13 in CSEA is >= 40 degF, then it is set to 1 Sensor 1: Is 0 unless either sensor 8 or 10 in CSSA is 1 then it is set to 1. Sensor 2: Is 0 unless any sensor in CSSC is 1 then it is set to 1 The following is a list of tables which are in this vidf TABLE 0: Ascii definitions of sensor states Units are simply instrument states. There are no alternate units Tony Lavoie Marshall Space Flight Center EL53 Huntsville, AL 35812 1 1996-02-25 08:20:03 1996-03-01 01:57:35 TSS : TSS-1Ro : DCORE : DCORE : DCDV DV/Autochk TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-25 08:19:58 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCDV DV/Voltage TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-25 08:19:58 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCDV DV/Autochk Active TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-25 08:19:58 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCDV DV/Overflow TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-25 08:19:58 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCDV DVG Pressure TSS:TSS-1:DCORE:DCORE:DCDV This virtual contains all of the data associated with the deployer DCORE voltmeter The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking sens 1 and 4 to volts TABLE 1: polymonial coefficients taking telemetry for sensor 4 to log(Torr) TABLE 2: decompress cal set 0 to give current sign TABLE 3: ascii definitions of values of sensor 2 TABLE 4: ascii definitions of cal set 0 data TABLE 5: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sensor 1 0 2 0 3 volts-dc Sensor 4 0 0 volts-dc Sensor 4 1 0 log(Torr) Cal 0 2 0 Sign of V Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 32 1996-02-25 08:19:58 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA1 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA2 I Set Echo TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA1 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA2 Tether I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA1 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA2 Anode I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA1 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA2 Filament I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA1 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DCORE : DCORE : DCGA EGA2 Coil I TSS:TSS-1:DCORE:DCORE:DCGA This virtual contains the some of the DCORE EGA current monitors. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry from sensors 0-5 to milliamps and from sensors 6-9 to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0-5 0 0 milliamps Sweep 6-9 0 0 amps Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 1 1996-02-25 08:20:01 1996-03-01 02:39:05 TSS : TSS-1Ro : DPLY : DPLY : DPMG Mea Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-25 08:19:59 1996-03-01 02:36:43 TSS : TSS-1Ro : DPLY : DPLY : DPMG Cmded Tether Len TSS:TSS-1:DPLY:DPLY:DPMG This virtual contains the commanded and measured tether length monitors. The tether length is spread out over the sensors and two calibration sets. The sensor holds the 1's and 10's places of the length and the cal sets the .1 and .01's and the 100's and 1000's places The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients cal set 0 to meters TABLE 1: polynomial coefficients cal set 1 to meters TABLE 2: polynomial coefficients converting meters to km The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep all 0 1 1 1 meters Sweep all 0 1 2 1 1 3 km Cal 0 0 0 meters Cal 1 1 0 meters Cal 0 0 2 0 3 km Cal 1 1 2 0 3 km Ron Geiger Martin Marietta Astronautics 12257 State Highway 121 Littleton, CO 80127 2 1996-02-25 08:19:59 1996-03-01 02:36:43 TSS : TSS-1Ro : RETE : RETE : RTAC AC-EF TSS:TSS-1:RETE:RETE:RTAC The RETE AC electric field measurements The following is a list of tables which are in this vidf TABLE 0: Lookup tables converting telemetry to volts for both high and low gain TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 volts Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-25 08:44:32 1996-03-01 04:59:26 TSS : TSS-1Ro : RETE : RETE : RTIP Ion Probe I TSS:TSS-1:RETE:RETE:RTIP The RETE ion probe current. The sensor is a simple electrostatic ion trap (Faraday Cup), biased at a fixed voltage of -7.5V with respect to the canaster. The following is a list of tables which are in this vidf TABLE 0: Lookup table converting telemetry to amps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENS TABLES OPERS UNIT Sensor 0 0 0 amps Sensor 0 1 0 nanoamps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-23 06:27:48 1996-03-01 07:44:54 TSS : TSS-1Ro : RETE : RETE : RTKE Pentode/I TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-25 08:28:08 1996-03-01 07:44:21 TSS : TSS-1Ro : RETE : RETE : RTKE DCBP/Pot TSS:TSS-1:RETE:RETE:RTKE The DC boom package is connected to the satellite ground via a pentode whose equivalent resistance can be varied to control either the DC canister potential or the current which is drawn from the canister to the satellite. This vidf returns the pentode current and the potential drop between the canister and the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients converting sensor data (micro-amps, volts) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 0 volts Sensor 1 0 0 micro-amps Dr. Marino Dobrowolny Instituto Di Fisica Dello Spazio Interplanetario Via G. Galilei - Casella Postale 27 Frascati, Italy 00044 1 1996-02-25 08:28:08 1996-03-01 07:44:21 TSS : TSS-1Ro : RETE : RETE : RTRLP Pnts Per Swp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Float Potential TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Plasma Potential TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Plasma Temp TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Min e- Den TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Max e- Den TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP p+ Den TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP IV Fit Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Float Pot Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Plasma Pot Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Plasma T Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Min e- Den Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP Max e- Den Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : RETE : RETE : RTRLP p+ Den Qual TSS:TSS-1:RETE:RETE:RTRLP This virtual contains reduced Langmuir Probe data. The virtual contains electron and ion densities, plasma temperatures, and plasma potentials. There are no tables associated with this virtual. All sensor data is stored in float format and have units attached The following units are associated with the sensors: SENSORS UNIT 0 unitless 1, 2 volts 3 degrees K 4, 5, 6 cm**-3 7, 8, 9, 10, 11, 12, 13 unitless 1 1996-02-23 07:00:34 1996-02-26 01:00:03 TSS : TSS-1Ro : ROPE : ROPE : RPBB BMSP I TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPBB Meas BMSP V TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPBB Cmd BMSP V TSS:TSS-1:ROPE:ROPE:RPBB This virtual contains the measured floating supply current and both the measured and commanded voltage needed to cancel the the local boom potential. The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (volts & current) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 microamps Sweep 1 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R Floating Supply Current and Voltage Needed to Cancel the Local Boom Potential. 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Num of Peaks TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 1: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 2: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 3: Loc TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 1: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 2: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDM Peak 3: 1/2I TSS:TSS-1:ROPE:ROPE:RPDM This virtual instrument contains the sweep step number of the 1/2 current level and peak voltage level of any peaks found in the difflection portion of the DIFP sweep The following is a list of tables which are in this vidf TABLE 0: table taking sweep step to volts TABLE 1: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 volts Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Peak Sweep Numbers and Deflection Voltages 4 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDP Defl TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDP Retard TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDP Retard/Pk 1 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDP Retard/Pk 2 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPDP Retard/Pk 3 TSS:TSS-1:ROPE:ROPE:RPDP A few leading comments. The instrument does not return a regular set of scan steps, instead, the scan step of each data sample is returned with it. To keep from writing a header record with each sweep, the sweep steps are returned in a calibration set and are obtained from here. In addition, the scan range can vary and these are distinguished by a critical action status byte attached to the table returning the scan voltages The following is a list of tables which are in this vidf TABLE 0: center energies (eV) (from calibration set) TABLE 1: telemetry decompression table TABLE 2: ascii definitions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 volts Sweep 1 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 TSS-1R ROPE DIFF Deflection and Retarding Current and Voltage 2 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPEB e- Sen 1 TSS:TSS-1:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1996-02-27 04:05:28 1996-02-27 04:05:28 TSS : TSS-1Ro : ROPE : ROPE : RPEB e- Sen 2 TSS:TSS-1:ROPE:ROPE:RPEB This virtual consists of data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Electron Senors 1 1996-02-27 04:05:28 1996-02-27 04:05:28 TSS : TSS-1Ro : ROPE : ROPE : RPEM Dif/Elec TSS : TSS-1 : ROPE : ROPE : RPEM This virtual instrument contains the DIFP electrometer data The following is a list of tables which are in this vidf TABLE 0: lookup table converting telemetry to amps The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 4 1996-02-23 06:33:00 1996-02-28 06:28:52 TSS : TSS-1Ro : ROPE : ROPE : RPHA FmtCntr/Lo TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA FmtCntr/Hi TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA Cyc/Cntr TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA Cmd/Word TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA DIFP-E/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA DIFP-S/T TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHA EPROM/Chksm TSS:TSS-1:ROPE:ROPE:RPHA This virtual contains some of the DIFP housekeeping data The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table for temps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 4,5 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB DifV -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB RtdV 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI 0VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI +/-25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI +/-50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI +/-75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI -/+75VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI -/+50VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI -/+25VD:0VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHB ColI 0VD:50VR TSS | TSS-1 | ROPE | ROPE | RPHB This virtual instrument contains the DIFP voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients and lookup table converting telemetry to volts or amps respectively. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-7 0 0 volts-dc 8-15 0 0 amps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 1 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 1 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 2 +V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 2 -V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 30V TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC HVPS 30V I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC PPS1 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHC PPS2 I TSS | TSS-1 | ROPE | ROPE | RPHC This virtual instrument contains the SPES voltage and current monitors The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to volts for sensors 0-4 and milliamps for sensors 5-9. The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-4 0 0 volts-dc 5-9 0 0 milli-amps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES1/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES2/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES3/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES4/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES5/e- GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES1/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES2/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES3/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES4/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHD SPES5/p+ GridV TSS | TSS-1 | ROPE | ROPE | RPHD This virtual instrument contains the SPES grid voltages The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT all 0 0 volts-dc Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP 0V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FS +28V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FS +5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FS +15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FS -15V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FS 5V TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE FPS T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE HVPS1 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE HVPS2 T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE CEP El T TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHE MF Cntr TSS | TSS-1 | ROPE | ROPE | RPHE This virtual instrument contains the CEP and Floating Supply voltage and temperature monitors. The ROPE major frame counter is also found within the virtual instrument The following is a list of tables which are in this vidf TABLE 0: Look up table taking telemetry to degrees C and polynomial coefficients taking telemetry to volts The following are units which can be derived from the tables. SENSORS TABLES OPERS UNIT 0-9 0 0 volts-dc 10-14 0 0 degrees C 15 - - integer Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dewsi.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPHG FPS I/Monitor TSS | TSS-1 | ROPE | ROPE | RPHG This virtual instrument contains the floating power supply (FPS) current monitor. The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients converting telemetry to uamps The following are units which can be derived from the tables. TYPE TABLES OPERS UNIT swp 0 0 microamps Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPIB p- Sen 1 TSS:TSS-1R:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1996-02-27 04:05:28 1996-02-27 04:05:28 TSS : TSS-1Ro : ROPE : ROPE : RPIB p- Sen 2 TSS:TSS-1R:ROPE:ROPE:RPIB This virtual consists of ion data from the two boom mounted SPES heads. Sensors point along a radial direction with sensor 0 pointing back at the satellite and sensor 1 pointing away from the satellite The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: 1/(detector efficiencies) TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: conversion factor taking eV to ergs TABLE 6: constant needed in going to dist. fn TABLE 7: table setting up statistical poisson corrections to cr TABLE 8: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNIT Scan 0 0 eV Sen 1 0 cnts/accum Sen 1,2 0,3 cnts/accum (eff. cor) Sen 1,2 0,153 cnts/sec Sen 1,2,3,4 0,153,4,4 cnts/(cm**2-str-s) Sen 1,2,3,4,0 0,153,4,4,4 cnts/(cm**2-str-s-eV) Sen 1,2,3,4,5 0,153,4,4,3 ergs/(cm**2-str-s-eV) Sen 1,2,3,4,6,5,0,5,0 0,153,4,4,3,4,4,4,4 sec**3/km**6 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu TSS-1R ROPE SPES Boom Mounted Ion Senors 1 1996-02-27 04:05:28 1996-02-27 04:05:28 TSS : TSS-1Ro : ROPE : ROPE : RPSA SPES 1 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA SPES 2 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA SPES 3 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA SPES 4 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA SPES 5 Grid TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA HVPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA HVPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA PPS 1 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSA PPS 2 State TSS:TSS-1:ROPE:ROPE:RPSA This virtual consists of the event flags for the SPES grid bias, and the high voltage power supplies. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states Units are simply instrument states. There are no alternate units Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@pemrac.space.swri.edu 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB FPS Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB FPS Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB FPS Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS1 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS1 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS1 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS2 Start Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS2 Skip Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB PPS2 Stop Step TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB HVU Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB Grid Bias Status TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB Macro Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB DIFP Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB FPS Cmds TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB Tele Test TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSB End Cmd TSS:TSS-1:ROPE:ROPE:RPSB This virtual consists of the ROPE command status words. There are no tables associated with this VIDF. Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Pot:Seek Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Pot:Track Mode TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Pot:Seek/Track Fail TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Pwr Comsump. TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Perf Pwr Consump Chk TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Bad Readings TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Bad FPS/V Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSC Bad BMSP/I Reading TSS:TSS-1:ROPE:ROPE:RPSC This virtual consists of the event flags for the FPS. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD RAM I/O Timer1: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD RAM I/O Timer1: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD RAM I/O Timer2: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD RAM I/O Timer2: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD 2K RAM: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD 2K RAM: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD 8K RAM: Tst 1 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : ROPE : ROPE : RPSD 8K RAM: Tst 2 TSS:TSS-1:ROPE:ROPE:RPSD This virtual consists of the DIFP RAM tests. The following is a list of tables which are in this vidf TABLE 0: ascii definitions of sensor states The telemetry had no tables associated with it to put it in any alternate units Dr. Nobie Stone Marshall Space Flight Center ES53 Huntsville, AL 35812 1 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK Yaw/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK Yaw/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK InPl/Rear TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK InPl/Frnt TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK OutPl/Right TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK OutPl/Left TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK InLn/V1 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SAHK : SAHK : SHSK InLn/V2 TSS:TSS-1:SAHK:SAHK:SHSK This virtual contains the satellite thruster monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions for thrusters Units are simply instrument states. There are no alternate units G. Oelker Alenia Spazio S.p.A. Corso MARCHE. 41 10146 Torino, Italia 1 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SCORE : SCORE : SCMC SV/Ovflow TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SCORE : SCORE : SCMC SV/Achk/S TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SCORE : SCORE : SCMC SV/AChk TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SCORE : SCORE : SCMC Tether/I TSS:TSS-1:SCORE:SCORE:SCMC This virtual contains all of the data associated with the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: telemetry decompression table (current) TABLE 1: decompress cal set 0 to give current sign TABLE 2: ascii definitions of values of sensors 0-2 TABLE 3: ascii definitions of cal set 0 data TABLE 4: ascii definitions of status bytes The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SENSOR TABLES OPERS UNIT Sweep 0 0 0 milliamps Sweep 1 0 0 volts-dc Carlo Bonifazi ASI V. Regina Margherita 202 00188 Roma, Italy 64 1996-02-25 08:20:01 1996-03-01 07:44:37 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Pwr TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB EGA Sync1 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB EGA Sync2 TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Enable Pulses Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Enable Off Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Enable On Tm Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Fila Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Fila Enable Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Fila On Tmr Set TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Fila On Disc TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG HV Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG HV Enable Var TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG HV Arm TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG HV On TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Run Bar Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Gun1 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Gun2 Select TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Run TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Stop TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Stret Gun Pulse TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Go Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Send Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Ready Cmd TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Cur Limit TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB FPEG Squel Enable TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STFB Gun Sw Pulse Mon TSS:TSS-1:SETS:SETS:STFB This virtual contains the SETS FPEG status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTA Tether I TSS:TSS-1:SETS:SETS:STTA This virtual contains the SETS tether current monitor. The following is a list of tables which are in this vidf TABLE 0: polynomial coefficients taking telemetry to amps TABLE 1: polynomial coefficients taking telemetry to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sweep 0 0 0 amps Sweep 0 1 0 milliamps Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 4 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Pwr TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/CAL A/C TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TVM/AC/FC TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TCM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TCM/LP/FR B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM TCM/LP/FR B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Mux Add B0 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Mux Add B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Mux Add B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Mux Add B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Hskp Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/Gain/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/Gain/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/LPFR/ B1 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/LPFR/ B2 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/LPFR/ B3 TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/CAL/-IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMM/CAL/+IR TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMS/Relay TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMS/DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM CMS/Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Shunt Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Shunt DOL TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Shunt Enable TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM 2.5 Mohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM 250 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM 25 Kohm TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM HV Prot TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD TCVM Mech Mode Sw TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SETS : SETS : STTD Prot Cap En Rly TSS:TSS-1:SETS:SETS:STTD This virtual contains the SETS TCVM relay status monitors. The following is a list of tables which are in this vidf TABLE 0: Ascii State definitions sensor states Units are simply instrument states. There are no alternate units Ivan Linscott Stanford University EERA/STAR Lab Durand Bldg, Rm 235 Stanford, CA 94305-4055 1 1996-02-24 02:51:47 1996-03-01 02:46:47 TSS : TSS-1Ro : SPREE : SPREE : SPOP Orb Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Conf Fac TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Head Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Zone Giving Pot TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Ch Above Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Peak Channel TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : SPREE : SPREE : SPOP Ch Below Peak TSS:TSS-1:SPREE:SPREE:SPOP This virtual contains the SPREE potential determination data. The following is a list of tables which are in this vidf TABLE 0: look up tables converting telemetry from sensor 0 to volts and from sensors 3-5 to cnts/accum. Polynomial coefficients converting telemetry from sensor 2 to integer TABLE 1: ascii definitions of status states The following are units which can be derived from the VIDF tables. The format is to give the tables applied followed by the operations and unit definition SENSOR TABLES OPERS UNIT 0 0 0 volts 1,6 - - integer 2 0 0 integer 3-5 0 0 cnts/accum Dr. Dave Hardy GL/PHE Hanscom A.F.B., MA 01731 4 1996-02-25 08:20:00 1996-03-01 02:45:06 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA Out/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA In/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA Ele/Temp TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA -8V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA +12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA -12V Sup TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA +5V Ref TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHA Spare TSS:TSS-1:TEMAG:TEMAG:TMHA This virtual contains the magnetometer housekeeping data The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to degrees for sensors 0-2 The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor 0-2 0,1 0,0 degrees C Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHB TeleCmd Echo TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:51 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMHB Chksum TSS:TSS-1:TEMAG:TEMAG:TMHB This virtual contains the magnetometer housekeeping data There are no tables associated with this vidf. All data is in its base units in its raw format. Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:51 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMI In/Bx TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 0: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMI In/By TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 0: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMI In/Bz TSS:TSS-1:TEMAG:TEMAG:TMMI This virtual contains inboard science magnetometer data. This magnetometer is located midway out on the fixed boom, about 50 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 0: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMO Out/Bx TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 1: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMO Out/By TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 1: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMMO Out/Bz TSS:TSS-1:TEMAG:TEMAG:TMMO This virtual contains outboard science magnetometer data. This magnetometer is located at the end of the fixed boom, about 100 cm from the satellite The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts the sensor data to nanotesla TABLE 1: Polynomial coefficients which converts the sensor data to gauss The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 0 0 nanotesla Sensor 1 0 gauss Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Inboard Science Magnetometer Data 8 1996-02-23 06:10:52 1996-03-01 07:44:37 TSS : TSS-1Ro : TEMAG : TEMAG : TMTA Tether Cur. TSS:TSS-1:TEMAG:TEMAG:TMTA This virtual contains the tether current data obtained from the satellite ampmeter The following is a list of tables which are in this vidf TABLE 0: Polynomial Coefficients taking telemetry to volts TABLE 1: Polynomial Coefficients taking volts to milliamps The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE SEN TABLES OPERS UNIT Sensor all 0 0 volts Sensor all 0,1 0,0 mamps Dr. Franco Mariani University of Vergata, Departmento Fisica E. Carnevale 00173 Roma, Italy TSS-1R TEMAG Tether Current Obtained from the Satellite Ampmeter 8 1996-02-23 06:10:52 1996-03-01 07:44:37 UARS : UARS-1 : CLAES : LEVEL_3AT : C2O5 CLAES/N2O5/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : C2O5 CLAES/N2O5/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : C3B8 CLAES/O3B8/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : C3B8 CLAES/O3B8/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : C3B9 CLAES/O3B9/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : C3B9 CLAES/O3B9/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CALT CLAES/Altitude The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Note that applying table 1 should generate a diagonal line if relation of the atmosphere used by CLAES is the same as the 1976 US Standard Atmosphere (which is used to generate the altitude conversion tables). Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CALT CLAES/Altitude/Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Note that applying table 1 should generate a diagonal line if relation of the atmosphere used by CLAES is the same as the 1976 US Standard Atmosphere (which is used to generate the altitude conversion tables). Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR2 CLAES/AERO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR2 CLAES/AERO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR3 CLAES/AERO3/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR3 CLAES/AERO3/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR4 CLAES/AERO4/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR4 CLAES/AERO4/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR8 CLAES/AERO8/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR8 CLAES/AERO8/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR9 CLAES/AERO9/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CAR9 CLAES/AERO9/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CCH4 CLAES/CH4/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CCH4 CLAES/CH4/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CCON CLAES/ClONO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CCON CLAES/ClONO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CH2O CLAES/H2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CH2O CLAES/H2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CN2O CLAES/N2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CN2O CLAES/N2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CNO2 CLAES/NO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CNO2 CLAES/NO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CNO_ CLAES/NO/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:01:58 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CNO_ CLAES/NO/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:01:58 1991-11-09 10:03:37 UARS : UARS-1 : CLAES : LEVEL_3AT : CTMP CLAES/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : CTMP CLAES/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:53 1991-11-09 10:02:31 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC2 Latitude/CLAES/AERO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC2 Longitude/CLAES/AERO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC2 LST/CLAES/AERO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC2 SZA/CLAES/AERO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC3 Latitude/CLAES/AERO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC3 Longitude/CLAES/AERO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC3 LST/CLAES/AERO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC3 SZA/CLAES/AERO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC4 Latitude/CLAES/AERO4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC4 Longitude/CLAES/AERO4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC4 LST/CLAES/AERO4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC4 SZA/CLAES/AERO4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC8 Latitude/CLAES/AERO8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC8 Longitude/CLAES/AERO8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC8 LST/CLAES/AERO8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC8 SZA/CLAES/AERO8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC9 Latitude/CLAES/AERO9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC9 Longitude/CLAES/AERO9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC9 LST/CLAES/AERO9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OAC9 SZA/CLAES/AERO9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACD Latitude/CLAES/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACD Longitude/CLAES/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACD LST/CLAES/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACD SZA/CLAES/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACG Latitude/CLAES/ALT Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACG Longitude/CLAES/ALT Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACG LST/CLAES/ALT Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACG SZA/CLAES/ALT Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACI Latitude/CLAES/C3B8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACI Longitude/CLAES/C3B8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACI LST/CLAES/C3B8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACI SZA/CLAES/C3B8 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACJ Latitude/CLAES/C3B9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACJ Longitude/CLAES/C3B9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACJ LST/CLAES/C3B9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACJ SZA/CLAES/C3B9 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACK Latitude/CLAES/ClONO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACK Longitude/CLAES/ClONO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACK LST/CLAES/ClONO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACK SZA/CLAES/ClONO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACM Latitude/CLAES/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACM Longitude/CLAES/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACM LST/CLAES/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACM SZA/CLAES/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACN Latitude/CLAES/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACN Longitude/CLAES/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACN LST/CLAES/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACN SZA/CLAES/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACO Latitude/CLAES/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:02:31 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACO Longitude/CLAES/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:02:31 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACO LST/CLAES/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:02:31 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACO SZA/CLAES/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:02:31 1991-11-09 10:04:10 UARS : UARS-1 : CLAES : LEVEL_3AT : OACQ Latitude/CLAES/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACQ Longitude/CLAES/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACQ LST/CLAES/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACQ SZA/CLAES/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACT Latitude/CLAES/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACT Longitude/CLAES/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACT LST/CLAES/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACT SZA/CLAES/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACW Latitude/CLAES/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACW Longitude/CLAES/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACW LST/CLAES/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : CLAES : LEVEL_3AT : OACW SZA/CLAES/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:01:25 1991-11-09 10:03:04 UARS : UARS-1 : HALOE : LEVEL_3AT : HCH4 HALOE/CH4/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HCH4 HALOE/CH4/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HH2O HALOE/H2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HH2O HALOE/H2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HHCL HALOE/HCl/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HHCL HALOE/HCl/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HNO2 HALOE/NO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HNO2 HALOE/NO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HNO_ HALOE/NO/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HNO_ HALOE/NO/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HO3_ HALOE/O3/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HO3_ HALOE/O3/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HTMP HALOE/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : HTMP HALOE/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-10-11 07:14:17 2001-10-22 09:37:53 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHC Latitude/HALOE/HCl Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHC Longitude/HALOE/HCl Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHC LST/HALOE/HCl Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHC SZA/HALOE/HCl Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHD Latitude/HALOE/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHD Longitude/HALOE/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHD LST/HALOE/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHD SZA/HALOE/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHM Latitude/HALOE/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHM Longitude/HALOE/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHM LST/HALOE/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHM SZA/HALOE/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHO Latitude/HALOE/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHO Longitude/HALOE/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHO LST/HALOE/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHO SZA/HALOE/NO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHT Latitude/HALOE/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHT Longitude/HALOE/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHT LST/HALOE/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHT SZA/HALOE/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHW Latitude/HALOE/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHW Longitude/HALOE/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHW LST/HALOE/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHW SZA/HALOE/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHZ Latitude/HALOE/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHZ Longitude/HALOE/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHZ LST/HALOE/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HALOE : LEVEL_3AT : OAHZ SZA/HALOE/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-10-11 07:14:50 2001-10-22 09:38:25 UARS : UARS-1 : HRDI : LEVEL_3AT : HRMA HRDI/Meridional/Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:10:55 1992-04-09 06:21:00 UARS : UARS-1 : HRDI : LEVEL_3AT : HRMA Std Dev HRDI Merid Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:10:55 1992-04-09 06:21:00 UARS : UARS-1 : HRDI : LEVEL_3AT : HRVA HRDI/Vol/Emission/Rate The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of photons/(cm**2-second). Table 0: UARS Altitudes for the reporting bins Table 1: Altitude converted Pressure Levels Table 2: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of photons/(cm**2-second). DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 1 0 Pressure (mbar) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 06:37:23 1992-04-09 06:37:23 UARS : UARS-1 : HRDI : LEVEL_3AT : HRVA Std Dev HRDI Emission Rate The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of photons/(cm**2-second). Table 0: UARS Altitudes for the reporting bins Table 1: Altitude converted Pressure Levels Table 2: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of photons/(cm**2-second). DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 1 0 Pressure (mbar) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 06:37:23 1992-04-09 06:37:23 UARS : UARS-1 : HRDI : LEVEL_3AT : HRZA HRDI/Zonal/Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:10:55 1992-04-09 06:21:00 UARS : UARS-1 : HRDI : LEVEL_3AT : HRZA Std Dev HRDI Zonal Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:10:55 1992-04-09 06:21:00 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMA Latitude/HRDI/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:11:28 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMA Longitude/HRDI/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:11:28 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMA LST/HRDI/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:11:28 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMA SZA/HRDI/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:11:28 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMP Latitude/HRDI/MP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMP Longitude/HRDI/MP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMP LST/HRDI/MP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRMP SZA/HRDI/MP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRPT Latitude/HRDI/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1993-11-01 12:07:05 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRPT Longitude/HRDI/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1993-11-01 12:07:05 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRPT LST/HRDI/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1993-11-01 12:07:05 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRPT SZA/HRDI/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1993-11-01 12:07:05 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVA Latitude/HRDI/VA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVA Longitude/HRDI/VA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVA LST/HRDI/VA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVA SZA/HRDI/VA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVP Latitude/HRDI/VP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVP Longitude/HRDI/VP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVP LST/HRDI/VP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRVP SZA/HRDI/VP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:09:26 1993-11-12 11:16:27 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZA Latitude/HRDI/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZA Longitude/HRDI/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZA LST/HRDI/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZA SZA/HRDI/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 10:38:14 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZP Latitude/HRDI/ZP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZP Longitude/HRDI/ZP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZP LST/HRDI/ZP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LRZP SZA/HRDI/ZP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-06 02:11:37 1993-11-13 11:21:55 UARS : UARS-1 : HRDI : LEVEL_3AT : LTMA HRDI/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1993-11-01 12:06:33 1993-11-12 10:02:44 UARS : UARS-1 : HRDI : LEVEL_3AT : LTMA HRDI/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1993-11-01 12:06:33 1993-11-12 10:02:44 UARS : UARS-1 : HRDI : LEVEL_3AT : LTMP HRDI/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to mbar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Pressures for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Pressure converted Altitude Levels Table 4: Pressure converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1993-11-01 12:06:33 1993-11-12 10:02:44 UARS : UARS-1 : HRDI : LEVEL_3AT : LTMP HRDI/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to mbar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Pressures for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Pressure converted Altitude Levels Table 4: Pressure converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1993-11-01 12:06:33 1993-11-12 10:02:44 UARS : UARS-1 : ISAMS : LEVEL_3AT : I121 ISAMS/AERO12P1/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : I121 ISAMS/AERO12P1/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : I2O5 ISAMS/N2O5/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : I2O5 ISAMS/N2O5/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : I623 ISAMS/AERO6P23/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : I623 ISAMS/AERO6P23/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ICH4 ISAMS/CH4/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ICH4 ISAMS/CH4/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ICO_ ISAMS/CO/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ICO_ ISAMS/CO/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : IH2O ISAMS/H2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:22:11 UARS : UARS-1 : ISAMS : LEVEL_3AT : IH2O ISAMS/H2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:22:11 UARS : UARS-1 : ISAMS : LEVEL_3AT : IN2O ISAMS/N2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : IN2O ISAMS/N2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : INAC ISAMS/HNO3/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : INAC ISAMS/HNO3/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : INO2 ISAMS/NO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : INO2 ISAMS/NO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : IO3_ ISAMS/O3/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : IO3_ ISAMS/O3/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ITMP ISAMS/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : ITMP ISAMS/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-08 11:59:47 1991-11-09 10:01:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI1 Latitude/ISAMS/AERO12P1 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI1 Longitude/ISAMS/AERO12P1 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI1 LST/ISAMS/AERO12P1 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI1 SZA/ISAMS/AERO12P1 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI6 Latitude/ISAMS/AERO6P23 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI6 Longitude/ISAMS/AERO6P23 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI6 LST/ISAMS/AERO6P23 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAI6 SZA/ISAMS/AERO6P23 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIA Latitude/ISAMS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIA Longitude/ISAMS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIA LST/ISAMS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIA SZA/ISAMS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:01:58 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIB Latitude/ISAMS/CO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIB Longitude/ISAMS/CO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIB LST/ISAMS/CO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIB SZA/ISAMS/CO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAID Latitude/ISAMS/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAID Longitude/ISAMS/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAID LST/ISAMS/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAID SZA/ISAMS/NO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIM Latitude/ISAMS/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIM Longitude/ISAMS/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIM LST/ISAMS/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIM SZA/ISAMS/CH4 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIN Latitude/ISAMS/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIN Longitude/ISAMS/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIN LST/ISAMS/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIN SZA/ISAMS/N2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIQ Latitude/ISAMS/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:23:49 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIQ Longitude/ISAMS/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:23:49 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIQ LST/ISAMS/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:23:49 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIQ SZA/ISAMS/N2O5 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:23:49 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIT Latitude/ISAMS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 09:51:03 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIT Longitude/ISAMS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 09:51:03 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIT LST/ISAMS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 09:51:03 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIT SZA/ISAMS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 09:51:03 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIW Latitude/ISAMS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:22:44 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIW Longitude/ISAMS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:22:44 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIW LST/ISAMS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:22:44 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIW SZA/ISAMS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:22:44 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIZ Latitude/ISAMS/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIZ Longitude/ISAMS/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIZ LST/ISAMS/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : ISAMS : LEVEL_3AT : OAIZ SZA/ISAMS/O3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1991-11-09 12:00:20 1991-11-09 10:07:26 UARS : UARS-1 : MLS : LEVEL_3AT : MCLO MLS/ClO/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS ClO Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MCLO MLS/ClO/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS ClO Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MH2O MLS/H2O/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS H2O Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-04-21 10:02:41 UARS : UARS-1 : MLS : LEVEL_3AT : MH2O MLS/H2O/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS H2O Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-04-21 10:02:41 UARS : UARS-1 : MLS : LEVEL_3AT : MNAC MLS/HNO3/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS HNO3 Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MNAC MLS/HNO3/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS HNO3 Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MO31 MLS/O3-183/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS O3 at 183 GHz Mixing Ratio Profile 1 1991-11-06 12:00:58 1991-11-11 10:01:44 UARS : UARS-1 : MLS : LEVEL_3AT : MO31 MLS/O3-183/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS O3 at 183 GHz Mixing Ratio Profile 1 1991-11-06 12:00:58 1991-11-11 10:01:44 UARS : UARS-1 : MLS : LEVEL_3AT : MO32 MLS/O3-205/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS O3 at 205 GHz Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MO32 MLS/O3-205/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS O3 at 205 GHz Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MSO2 MLS/SO2/Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS SO2 Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MSO2 MLS/SO2/Std Dev Mix Ratio The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data is stored as a mixing ratio value. Table 00: pressure look-up table Table 01: pressure converted altitude Table 02: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as Mixing Ratio in units of Gas Molecule/Air Molecule DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 1 0 Altitude (km) Scan 2 0 Geopotential Altitude (km) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS SO2 Mixing Ratio Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MTMP MLS/Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Atmospheric Temperature Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : MTMP MLS/Std Dev Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to millibar). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 00: pressure look-up table Table 01: conversion from degrees K to degrees C Table 02: conversion from degrees C to degrees F Table 03: pressure converted altitude Table 04: pressure converted geopotential height Storage: Scan references UARS pressure bin number Sweep is stored as absolute temperature (degrees K) DATA TYPE TABLES OPERS UNIT Scan 0 0 Pressure (mbar) Scan 3 0 Altitude (km) Scan 4 0 Geopotential Altitude (km) Sweep 1 1 degrees C Sweep 1,2 1,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Atmospheric Temperature Profile 1 1991-11-06 12:00:58 1993-11-13 10:02:43 UARS : UARS-1 : MLS : LEVEL_3AT : OAM1 Latitude/MLS/O3_183 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 183 GHz Measurement 60 1991-11-06 12:01:30 1991-11-11 09:51:22 UARS : UARS-1 : MLS : LEVEL_3AT : OAM1 Longitude/MLS/O3_183 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 183 GHz Measurement 60 1991-11-06 12:01:30 1991-11-11 09:51:22 UARS : UARS-1 : MLS : LEVEL_3AT : OAM1 LST/MLS/O3_183 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 183 GHz Measurement 60 1991-11-06 12:01:30 1991-11-11 09:51:22 UARS : UARS-1 : MLS : LEVEL_3AT : OAM1 SZA/MLS/O3_183 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 183 GHz Measurement 60 1991-11-06 12:01:30 1991-11-11 09:51:22 UARS : UARS-1 : MLS : LEVEL_3AT : OAM2 Latitude/MLS/O3_205 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 205 GHz Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAM2 Longitude/MLS/O3_205 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 205 GHz Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAM2 LST/MLS/O3_205 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 205 GHz Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAM2 SZA/MLS/O3_205 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the O3 205 GHz Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMA Latitude/MLS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the HNO3 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMA Longitude/MLS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the HNO3 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMA LST/MLS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the HNO3 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMA SZA/MLS/HNO3 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the HNO3 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAML Latitude/MLS/ClO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the ClO Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAML Longitude/MLS/ClO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the ClO Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAML LST/MLS/ClO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the ClO Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAML SZA/MLS/ClO Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the ClO Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMS Latitude/MLS/SO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the SO2 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMS Longitude/MLS/SO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the SO2 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMS LST/MLS/SO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the SO2 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMS SZA/MLS/SO2 Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the SO2 Measurement 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMT Latitude/MLS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMT Longitude/MLS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMT LST/MLS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMT SZA/MLS/TMP Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 12:01:30 1993-11-13 09:52:20 UARS : UARS-1 : MLS : LEVEL_3AT : OAMW Latitude/MLS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the H2O Measurement 60 1991-11-06 12:01:30 1993-04-21 09:52:18 UARS : UARS-1 : MLS : LEVEL_3AT : OAMW Longitude/MLS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the H2O Measurement 60 1991-11-06 12:01:30 1993-04-21 09:52:18 UARS : UARS-1 : MLS : LEVEL_3AT : OAMW LST/MLS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the H2O Measurement 60 1991-11-06 12:01:30 1993-04-21 09:52:18 UARS : UARS-1 : MLS : LEVEL_3AT : OAMW SZA/MLS/H2O Position is the geographic location of the foot of the limb viewing point. Field Limb View Latitude is stored in degrees Field Limb View Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS MLS Earth Pointing Position for the H2O Measurement 60 1991-11-06 12:01:30 1993-04-21 09:52:18 UARS : UARS-1 : OAUR : OAUR : OAUR Att/VN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb1/VN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb2/VN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb3/VN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Att/CN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb1/CN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb2/CN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb3/CN This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Epoch/Y This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Epoch/D This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Epoch/Ms This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/Beg/Y This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/Beg/D This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/Beg/Ms This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/End/Y This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/End/D This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb/End/Ms This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Yaw This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Pitch This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Roll This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A11 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A21 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A31 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A12 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A22 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A32 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A13 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A23 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Rot-Elem/A33 This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Rx This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Ry This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Rz This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Vx This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Vy This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Vz This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Semi-Mj Axis This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Eccentricity This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Inclination This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR RA-Ascend Node This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Arg of Perigee This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Mean Anomaly This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR d(RA-Ascend Node)/dt This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR d(Arg of Perigee)/dt This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Mean Motion This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Nodal Period This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Orb # This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Sun/X This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Sun/Y This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR ECI/Sun/Z This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Earth/Sun Dis This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Gwich App Sid Tm This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Geod Lat This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR E Long This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Geod Alt This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR Earth Geod Rad This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR IL (100km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR IL (250km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR IL (600km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MLat (100km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MLat (250km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MLat (600km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MST (100km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MST (250km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR MST (600km) This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR SZA This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR LST This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : OAUR : OAUR : OAUR S Atl Anom This virtual contains all of the orbit/attitude parameters for the UARS satellite on 2 second centers Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS Spacecraft Orbit and Attitude Data 16 1991-09-15 12:53:01 2005-12-14 10:10:43 UARS : UARS-1 : PEM : AXIS : AXDA A1/P1/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P2/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P3/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P4/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P5/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P6/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P7/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/P8/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P1/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P2/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P3/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P4/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P5/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P6/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P7/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/P8/Energy Processor Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Command Buffer Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Unrecognized Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Unrecognized Clear/Set Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Bad Checksum No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Address-Low Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Address-High Command Sequencing No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/EOT Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Command Buffer Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Unrecognized Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Unrecognized Clear/Set Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Bad Checksum No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Address-Low Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Address-High Command Sequencing No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/EOT Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Bias Adjust Failure No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Bias Arm Without Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Bias On Not After Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Invalid Bias Arm Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Invalid Bias On Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Bias Adjust Failure No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Bias Arm Without Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Bias On Not After Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Invalid Bias Arm Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Invalid Bias On Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Invalid Mode Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Mode Command Without Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Invalid Mode Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Mode Command Without Arm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Bad Ram Load No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/RAM Load Buffer Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/RAM Load Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Unknown RAM Load Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Bad Ram Load No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/RAM Load Buffer Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/RAM Load Command Error No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Unknown RAM Load Command No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/New SMAF Before Loop No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/New PHA Before Accumulate No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/New SMAF Before Loop No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/New PHA Before Accumulate No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Mode Command Armed No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Echo Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Warm Start Enabled No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Watchdog Time Enabled No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Source Channel Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Jump Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A1/Microcomputer Memory Dump No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Mode Command Armed No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Echo Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Warm Start Enabled No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Watchdog Time Enabled No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Source Channel Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Jump Mode No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDA A2/Microcomputer Memory Dump No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Bias Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Level Control, Bias A No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Level Control, Bias B No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Bias A Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Bias B Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Bias Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Level Control, Bias A No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Level Control, Bias B No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Bias A Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Bias B Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Calibration Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Calibration Pulser No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A1/Cal. Running|Pending No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Calibration Enable No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Calibration Pulser No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXDB A2/Cal. Running|Pending No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHA A1/Command Counter No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHA A2/Command Counter No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHA A1/Microcomp. Warm/Start/Cnt No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHA A2/Microcomp. Warm/Start/Cnt No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Address/Low Byte No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Address/High Byte No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Address/Low Byte No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Address/High Byte No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 1 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 2 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 3 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 4 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 5 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 6 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 7 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 8 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 9 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 10 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 11 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 12 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 13 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 14 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 15 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 16 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 17 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 18 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A1/Memory Byte 19 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 1 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 2 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 3 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 4 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 5 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 6 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 7 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 8 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 9 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 10 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 11 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 12 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 13 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 14 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 15 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 16 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 17 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 18 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHB A2/Memory Byte 19 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P1/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P2/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P3/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P4/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P5/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P6/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P7/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P8/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P1/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P2/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P3/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P4/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P5/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P6/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P7/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P8/Detector Singles No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P1/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P2/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P3/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P4/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P5/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P6/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P7/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P8/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P1/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P2/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P3/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P4/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P5/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P6/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P7/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P8/Integrator Overflow No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P1/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P2/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P3/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P4/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P5/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P6/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P7/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A1/P8/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P1/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P2/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P3/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P4/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P5/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P6/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P7/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHC A2/P8/Inhibit No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS PEM AXIS Singles cound of its X-ray Pixels 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHD A1/Main Pwr Supply Current No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/Main Pwr Supply Current No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/Bias Supply 1 Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/Bias Supply 2 Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/Bias Supply 1 Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/Bias Supply 2 Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/+5 V Ref. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/+5 V Dig. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/+5 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/+6 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/-6 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/-12 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/+26 V Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/+5 V Ref. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/+5 V Dig. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/+5 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/+6 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/-6 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/-12 V Ana. Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/+26 V Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/Preamp Base Plate Temp. No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/T-beam Temperature, Cold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A1/T-beam Temperature, Warm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/Preamp Base Plate Temp. No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/T-beam Temperature, Cold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD A2/T-beam Temperature, Warm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Electronics Box Temperature No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Base Plate Temperature No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Sensor Housing Temperature No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Radiator Primary Temp., Cold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Radiator Primary Temp., Warm No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHD Radiator Secondary Temp. No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:27 2005-03-08 12:25:32 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP0/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP2/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP4/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP6/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP8/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP10/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP12/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP14/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP0/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP2/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP4/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP6/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP8/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP10/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP12/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP14/Pileup Register No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP0/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP2/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP4/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP6/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP8/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP10/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP12/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP14/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP0/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP2/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP4/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP6/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP8/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP10/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP12/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP14/Lower Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP0/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP2/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP4/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP6/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP8/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP10/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP12/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A1/EP14/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP0/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP2/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP4/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP6/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP8/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP10/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP12/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXHE A2/EP14/Upper Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-09-15 08:40:02 2005-03-08 12:25:07 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P1 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P2 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P3 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P4 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P5 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P6 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P7 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 1 P8 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P1 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P2 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P3 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P4 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P5 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P6 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P7 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSA AXIS 2 P8 UARS:UARS-1:PEM:AXIS:AXSA This VIDF defines the high energy resolution data of the AXIS portion of the PEM experiment. Data are returned in 32 energy bins from all 16 detectors every 8.192 seconds. The data is strongly contaminated by galactic cosmic rays and at times there is significant contamination from protons above 50 keV and electrons above 500-600 keV. A background subtraction technique is applied to the data to reduce the contamination. The subtraction is emperical. What appears to be a universal spectrum created by high energy protons and electrons normalized to the countrate found in either energy channels 19-21 or 28-28 is subtracted from the data. The latter range can be selected by the user when applying the correction. The galactic cosmic rays are removed by subtracting an emperical spectrum which varies with L-shell. In addition to the data the IDFS also contains the projection of each sensors look angles in geographic coordinates to the 100 km altitude. These are contained in calibration sets 3-8 and contain the outer edge, center, and inner edge longitude and latitude definitions for each sensor and are used when displaying the AXIS data in image format. Also in this VIDF are the total counts accumulated in each detector during each sweep (cat set 1) which is used in the dead time correction, and the average counts in the energy channels 19-21 (cal set 9), the average counts in energy channels 26-28 (cal set 10) and the L-shell value (cal set 11) which is used to remove the galactic cosmic ray background The tables contained in this VIDF are listed below, as are the included constants. There is a distinct division in the tables between those which describe the instrument characteristics and those needed for the background and dead time corrections. TABLE 0: telemetry decom table giving cnts/accum period TABLE 1: center energies in eV (1 set / sensor head) TABLE 2: energy channel widths in eV (1 set / sensor head) TABLE 3: detector efficiencies (1 / sensor head) TABLE 4: geometry factors in cm**2-str (1/sensor head) TABLE 5: conversion factor taking eV to ergs TABLE 6: telemetry decom table giving total accumulated counts and used with calibration set 2 TABLE 7: negative of energy processor repolling time (sec) TABLE 8: constant value (1) TABLE 9: converts cal set 3 to outer pixel longitude (deg) TABLE 10: converts cal set 4 to outer pixel latitude (deg) TABLE 11: converts cal set 5 to center pixel longitude (deg) TABLE 12: converts cal set 6 to center pixel latitude (deg) TABLE 13: converts cal set 7 to inner pixel longitude (deg) TABLE 14: converts cal set 8 to inner pixel latitude (deg) TABLE 15: galactic cosmic ray background correction spectra used in conjunction with the mode value. The sepctra give discrete corrections each 1/2 L value TABLE 16: converts cal set 9 to counts per second TABLE 17: converts cal set 10 to counts per second TABLE 18: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (Used in conjunction with cal set 9) TABLE 19: converts cal set 11 to L-Shell value TABLE 20: Polynomial coefficients (1 set / energy step / sensor) giving the galactic cosmic ray background correction as a function of L-Shell. (Used in conjunction with cal set 11) TABLE 21: universal spectra for penetrating hi energy particles as counts /sec (no efficiency correction) / incident particle (used in conjunction with cal set 10) TABLE 22: polynomial coefficients to load in the 1-count thresh. TABLE 23: converts mode 0 to L-Shell value CONST 1: X normal unit vector coordinates (UARS Coord) CONST 2: Y normal unit vector coordinates (UARS Coord) CONST 3: Z normal unit vector coordinates (UARS Coord) The following are units which can be derived from the tables. Because of the background subtraction then can be quite detailed and agre given at several levels. The first is the standard units with no background subtraction. Some short hand notations will be used to designate sequences of tables and operations. These are defined below: SYM TABLES OPERS DEFINITION --- ----------- ------------- ------------------- T 6,7,8,6,7 0,153,21,4,4 1 / live time (1/sec) EC 0,3,4 3,4,4 eff cor (cnts/cm**2-str) DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp T T live time (sec) Swp 0 0 cnts/accum Swp 0, 3 0, 4 cnts/accum (eff cor) Swp T, 0, 3 T, 3, 4 cnts/sec Swp T, EC, 1, 2 T, EC, 3, 4 cnts/(cm**2-str-s) Swp T, EC, 2 T, EC, 4 cnts/(cm**2-str-s-eV) Swp T, EC, 2, 5 T, EC, 4, 3 ergs/(cm**2-str-s-eV) Cal 2 6 6 total cnts Cal 3 9 0 degrees Cal 4 10 0 degrees Cal 5 11 0 degrees Cal 6 12 0 degrees Cal 7 13 0 degrees Cal 8 14 0 degrees Cal 9 16 0 total cnts Cal 10 17 0 total cnts Cal 11 19 0 L-Shell Mode 0 22 0 L-shell The following units are derived from the above and have both the GCR and the high energy backgrounds removed. The GCR background removal, given the acronym GR, can follow any one of 3 formalisms: remove spectrum according to TABLE 20, which uses a continuous GCR spectrum based on the L-Shell value given in cal set 11 (GR1), the removal of this spectra plus a 1 sigma deviation (GR2), or the the descrete GCR spectra accumulated every 1/2 L-shell unit and contained in TABLE 15 (GR3). The units definitions will only show GR which represents for one of the three methods defined above. There are also two methods to remove the high energy background. It can be accomplished by using either the average counts in energy channels 19-21 (HE1) as a basis or the average counts in energy channels 26-28 (HE2). The units as stated will only show HE which represents for one of the two methods defined above. SYM TABLES OPERS DEFINITION ---- ----------- ----------------------------- ---------------- T 6,7,8,6,7,0 1000,1153,1021,1004,1004,2003 1 / live time HE1 16,18,0 0,0,162 cnts-HE (19-21) HE2 17,22,0 0,0,162 cnts-HE (26-28) GCR1 20 2 GCR GCR2 20,20,0 1060,1001,2002 GCG + GCR**1/2 GCR3 15 2 GCG DATA TABLES OPERS UNITS ---- -------------- ---------------- ---------------------- Swp HE,T,GCR HE,T,GCR counts/sec Swp HE,T,GCR, 1, 2 HE,T,GCR, 3, 4 cnts/(cm**2-str-s) Swp HE,T,GCR, 2 HE,T,GCR, 4 cnts/(cm**2-str-s-eV) Swp HE,T,GCR, 2, 5 HE,T,GCR, 4, 3 ergs/(cm**2-str-s-eV) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu UARS PEM AXIS X-ray Data 8 1991-09-15 08:40:10 2005-03-08 09:21:21 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P3 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P4 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P5 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P6 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P7 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 1 P8 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P3 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P4 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P5 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P6 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P7 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSB AXIS 2 P8 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Scan 1 0 eV (center) Scan 2 0 eV (widths) Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 64 1991-09-15 08:40:17 2005-03-08 12:26:16 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/1/P1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/1/P2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/1/P3 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/1/P4 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/1/P5 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/2/P1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/2/P2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/2/P3 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/2/P4 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : AXIS : AXSC AXIS/2/P5 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TABLES OPERS UNITS Swp 0 0 cnts/accum Cal 0 6 total cnts Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 128 1991-09-15 08:40:02 2005-03-08 12:26:01 UARS : UARS-1 : PEM : EDEP : ED11 ED11 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED11 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-1, which were computed on the UARS CDHF. A ED11 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED11 ED11 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED11 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-1, which were computed on the UARS CDHF. A ED11 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED12 ED12 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED12 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-2, which were computed on the UARS CDHF. A ED12 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED12 ED12 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED12 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-2, which were computed on the UARS CDHF. A ED12 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED13 ED13 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED13 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-3, which were computed on the UARS CDHF. A ED13 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED13 ED13 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED13 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-3, which were computed on the UARS CDHF. A ED13 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED14 ED14 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED14 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-4, which were computed on the UARS CDHF. A ED14 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED14 ED14 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED14 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-4, which were computed on the UARS CDHF. A ED14 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED15 ED15 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED15 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-5, which were computed on the UARS CDHF. A ED15 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED15 ED15 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED15 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-5, which were computed on the UARS CDHF. A ED15 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED16 ED16 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED16 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-6, which were computed on the UARS CDHF. A ED16 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:01:23 1993-11-12 10:08:34 UARS : UARS-1 : PEM : EDEP : ED16 ED16 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED16 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-6, which were computed on the UARS CDHF. A ED16 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:01:23 1993-11-12 10:08:34 UARS : UARS-1 : PEM : EDEP : ED17 ED17 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED17 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-7, which were computed on the UARS CDHF. A ED17 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED17 ED17 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED17 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-7, which were computed on the UARS CDHF. A ED17 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED18 ED18 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED18 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-8, which were computed on the UARS CDHF. A ED18 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED18 ED18 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED18 is the X-ray reconstructed Electron Energy Deposition file from AXIS-1, Pixel-8, which were computed on the UARS CDHF. A ED18 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:07:28 UARS : UARS-1 : PEM : EDEP : ED21 ED21 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED21 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-1, which were computed on the UARS CDHF. A ED21 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED21 ED21 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED21 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-1, which were computed on the UARS CDHF. A ED21 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED22 ED22 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED22 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-2, which were computed on the UARS CDHF. A ED22 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:03:06 UARS : UARS-1 : PEM : EDEP : ED22 ED22 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED22 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-2, which were computed on the UARS CDHF. A ED22 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:03:06 UARS : UARS-1 : PEM : EDEP : ED23 ED23 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED23 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-3, which were computed on the UARS CDHF. A ED23 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:03:06 UARS : UARS-1 : PEM : EDEP : ED23 ED23 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED23 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-3, which were computed on the UARS CDHF. A ED23 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:03:06 UARS : UARS-1 : PEM : EDEP : ED24 ED24 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED24 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-4, which were computed on the UARS CDHF. A ED24 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED24 ED24 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED24 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-4, which were computed on the UARS CDHF. A ED24 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED25 ED25 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED25 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-5, which were computed on the UARS CDHF. A ED25 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED25 ED25 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED25 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-5, which were computed on the UARS CDHF. A ED25 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED26 ED26 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED26 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-6, which were computed on the UARS CDHF. A ED26 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED26 ED26 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED26 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-6, which were computed on the UARS CDHF. A ED26 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED27 ED27 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED27 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-7, which were computed on the UARS CDHF. A ED27 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED27 ED27 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED27 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-7, which were computed on the UARS CDHF. A ED27 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED28 ED28 The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED28 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-8, which were computed on the UARS CDHF. A ED28 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : ED28 ED28 Stand. Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of keV/(g-sec), the atmosphere independent energy deposition rate. Table 1 converts the rate using the US standard atmosphere which was used to generate the HEPS/MEPS floating point energy deposition values. Table 00: altitude look-up table Table 01: US Standard Atmospheric Mass Density Table 02: keV to eV conversion Table 03: average energy for each ionization Table 04: ionization fraction of N2+ Table 05: ionization fraction of N+ Table 06: ionization fraction of O2+ Table 07: ionization fraction of O+ Table 08: eV to ergs conversion Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of keV/(g-sec) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 3 keV / (cm**3-s) Sweep 1,2 3,3 eV / (cm**3-s) Sweep 1,2,3 3,3,4 ionizations / (cm**3-s) Sweep 1,2,3,4 3,3,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,3,5 3,3,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,3,6 3,3,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,3,7 3,3,4,3 ionizations of O+ / (cm**3-s) Sweep 1,2,8 3,3,3 erg / (cm**3-s) ED28 is the X-ray reconstructed Electron Energy Deposition file from AXIS-2, Pixel-8, which were computed on the UARS CDHF. A ED28 profile is computed once per UARS minute. The profile is generated by inferring the electron population which impacted on the atmosphere in order to produce the detected x-ray emission as seen by AXIS. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1993-11-12 10:02:01 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P1/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P2/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P3/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P4/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P5/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P6/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P7/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A1/P8/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P1/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P2/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P3/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P4/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P5/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P6/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P7/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Latitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Longitude This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Int/XRay/Flux This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Min/CHI**2 This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Corr/Int/Time This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/SD/Int/Dwn/Elect/Flx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/SD/Elect/e-Fold/Eng This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/SD/Hard/XRay/Bkgnd This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Elec/Fit/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Elect/Fit/SD/Indx This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Min/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Num/Eng/Chan/Used This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Peak/Ionz/Alt This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDA1 A2/P8/SD/Peak/Ionz This file contains the results of fitting AXIS pixels on the UARS CDHF. For each AXIS Pixel, the following parameters are recorded: Latitude is stored in degrees Longitude is stored in degrees Integrated X-Ray Flux is stored in units of photons/(cm**2-s-sr) Minimum $chi sup 2$ is a dimensionless parameter Corrected Integration Time is stored in seconds Integrated Downward Electron Flux is stored as electrons/(cm**2-s) Electron e-Folding Energy is stored in units of keV Hard X-Ray Background Magnitude is stored as counts/channel/s Std. Dev. of Integ. Downward Electron Flux stored as electrons/(cm**2-s) Std. Dev. of the Electron e-Folding Energy is stored in units of keV Std. Dev. of Hard X-Ray Background Magnitude stored as counts/channel/s Index for Fit is a dimensionless parameter Index for Fit Standard Deviation is a dimensionless parameter Minimum Channel Used to FIT is a dimensionless parameter Number of Energy Channels Used to FIT is a dimensionless parameter Altitude of Peak Ionization is stored in units of km Peak Ionization is stored in units of ionizations/(cm**3-s) Std. Dev. of Peak Ionization is stored in units of ionizations/(cm**3-s) The quantities recorded here are the UARS minute averaged values. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1997-02-16 10:01:55 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE HEPS Elect Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFE Stand Dev Fit The HEPS electron spectra that was determined by a fitting process which generated these paramaters. After deriving the fit, the standard energies were used with the the fit paramaters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The paramaters of the fit equation are stored as calibration paramaters. Two additional fit paramaters are stored as calibration paramaters. These are refered to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma accross spectra are not accurate. To get around this problem, the chi squared was also computed. Here, compairsons can be made with this paramater accross spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS electron energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Electron Energies (eV) [#*100] 47100 39300 33000 28100 23200 19300 16400 14000 12000 10050 8100 6600 5650 4750 3850 3200 2905 2555 2235 1945 1680 1445 1240 1065 920 805 690 575 490 430 370 315 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP HEPS Prot Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDFP Stand Dev Fit The HEPS proton spectra was determined by a fitting process which generated these parameters. After deriving the fit, the standard energies were used with the fit parameters to achieve the hemispherical flux. The data can have either a convex or concave shape. Spectra are fit in log-log space simulating a single power law, double power law, and iterated double power law. For the convex shape, the equation form is J1*(E**G1) + J2*(E**G2), where J1 and J2 are the amplitude terms while G1 and G2 are the powers. Here, E represents the MeV energy value (standard energy in eV divided by 10**6). When the shape is concave, the form of the reconstruction equation is 1000/[J1*(E**-G1) + J2*(E**-G2)]. Equation type is stored as a mode variable. The parameters of the fit equation are stored as regular data. Two additional fit parameters are also stored as regular data These are referred to as sigma and chi2. Sigma is an internal unnormalized goodness of fit indicator which is valid only for a spectra and was used in the decision over what type of equation should be used. Comparisons of sigma across spectra are not accurate. To get around this problem, the chi squared was also computed. Here, comparisons can be made with this parameter across spectra. It is a normalized value. The conversion to various units is accomplished by the application of different sets of look up tables once these coefficients are applied to the standard energies. This is described below (note table 0 describes the standard energies used in the fitting process). Reconstruction of the fit spectra require the use of an SCF. Tables are provided in this VIDF for use in that SCF. Table 00: standard HEPS proton energies Table 01: conversion factor, eV to ergs Storage: Fit First Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit Second Amplitude in in units of cnts/(cm**s-s-sr-eV) Fit First Power is a unitless number Fit Second Power is a unitless number Fit Internal Sigma is a unitless number Fit Chi Squared is a unitless number Fit Type is a unitless number Standard Proton Energies (eV) [#*1000] 141000 124000 107750 92750 78000 63750 53600 47350 40100 29900 21550 15050 11150 8200 6250 5300 4420 3250 2385 1725 1250 967 785 607 445 328 244 179 133 106 87 73 Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDHE HEPS Elec Energy Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDHE is the Energy Deposition for HEPS Electrons computed on the UARS CDHF for data averaged 1 minute and fitted to a double power law. HEPS energy sweep is 8 seconds for electrons, but one averaged data is used to compute the profile. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDHE HEPS Elec Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDHE is the Energy Deposition for HEPS Electrons computed on the UARS CDHF for data averaged 1 minute and fitted to a double power law. HEPS energy sweep is 8 seconds for electrons, but one averaged data is used to compute the profile. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDHP HEPS Prot Energy Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDHP is the Energy Deposition for HEPS Protons computed on the UARS CDHF for data averaged 1 minute and fitted to a double power law. HEPS energy sweep is 16 seconds for protons, but one averaged data is used to compute the profile. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDHP HEPS Prot Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDHP is the Energy Deposition for HEPS Protons computed on the UARS CDHF for data averaged 1 minute and fitted to a double power law. HEPS energy sweep is 16 seconds for protons, but one averaged data is used to compute the profile. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:00:18 1992-10-15 10:03:12 UARS : UARS-1 : PEM : EDEP : EDJE HEPS/MEPS Elec Eng Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDJE is the Energy Deposition file from Joint Electron data, combining the profiles from both HEPS and MEPS which were computed on the UARS CDHF. A EDJE profile is computed once per UARS minute. The MEPS profile is the average of the 2 second profiles generated for MEPS, computed every minute. The HEPS profile averages the HEPS counts for one minute, fits the data to a double power law, and then computes the profile. EDJE is a straight sum of both the HEPS and MEPS profiles. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:26:31 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : EDJE HEPS/MEPS Elec Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDJE is the Energy Deposition file from Joint Electron data, combining the profiles from both HEPS and MEPS which were computed on the UARS CDHF. A EDJE profile is computed once per UARS minute. The MEPS profile is the average of the 2 second profiles generated for MEPS, computed every minute. The HEPS profile averages the HEPS counts for one minute, fits the data to a double power law, and then computes the profile. EDJE is a straight sum of both the HEPS and MEPS profiles. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:26:31 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : EDJP HEPS/MEPS Prot Eng Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDJP is the Energy Deposition file from Joint Proton data, combining the profiles from both HEPS and MEPS which were computed on the UARS CDHF. A EDJP profile is computed once per UARS minute. The MEPS profile is the average of the 2 second profiles generated for MEPS, computed every minute. The HEPS profile averages the HEPS counts for one minute, fits the data to a double power law, and then computes the profile. EDJP is a straight sum of both the HEPS and MEPS profiles. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:26:31 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : EDJP HEPS/MEPS Prot Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDJP is the Energy Deposition file from Joint Proton data, combining the profiles from both HEPS and MEPS which were computed on the UARS CDHF. A EDJP profile is computed once per UARS minute. The MEPS profile is the average of the 2 second profiles generated for MEPS, computed every minute. The HEPS profile averages the HEPS counts for one minute, fits the data to a double power law, and then computes the profile. EDJP is a straight sum of both the HEPS and MEPS profiles. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1992-04-09 12:26:31 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : EDME MEPS Elec Energy Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDME is the Energy Deposition for MEPS Electrons computed on the UARS CDHF for each 2 second MEPS energy sweep Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 32 1992-04-09 12:27:36 1992-10-15 10:45:48 UARS : UARS-1 : PEM : EDEP : EDME MEPS Elec Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDME is the Energy Deposition for MEPS Electrons computed on the UARS CDHF for each 2 second MEPS energy sweep Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 32 1992-04-09 12:27:36 1992-10-15 10:45:48 UARS : UARS-1 : PEM : EDEP : EDMP MEPS Prot Energy Dep The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDMP is the Energy Deposition for MEPS Protons computed on the UARS CDHF for each 2 second MEPS energy sweep Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 32 1992-04-09 12:27:36 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : EDMP MEPS Prot Eng Dep Std Dev The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of ergs/(cm**3-sec), the energy deposition rate. Table 1 converts the floating point energy deposition values to determine the number of ionizations which occur [ionizations/(cm**3-sec)]. Table 00: altitude look-up table Table 01: ergs to eV conversion Table 02: average energy for each ionization Table 03: ionization fraction of N2+ Table 04: ionization fraction of N+ Table 05: ionization fraction of O2+ Table 06: ionization fraction of O+ Table 07: eV to keV conversion Table 08: US Standard Atmospheric Mass Density Table 09: altitude converted pressure Table 10: altitude converted geopotential height Storage: Scan references UARS altitude bin number Sweep is stored in units of erg/(cm**3-s) DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 9 0 Pressure (mbar) Scan 10 0 Geopotential Altitude (km) Sweep 1 4 eV / (cm**3-s) Sweep 1,2 4,4 ionizations / (cm**3-s) Sweep 1,2,3 4,4,3 ionizations of N2+ / (cm**3-s) Sweep 1,2,4 4,4,3 ionizations of N+ / (cm**3-s) Sweep 1,2,5 4,4,3 ionizations of O2+ / (cm**3-s) Sweep 1,2,6 4,4,3 ionizations of O+ / (cm**3-s) Sweep 1,7 4,4 keV / (cm**3-s) Sweep 1,7,8 4,4,4 keV / (g-s) EDMP is the Energy Deposition for MEPS Protons computed on the UARS CDHF for each 2 second MEPS energy sweep Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 32 1992-04-09 12:27:36 1992-10-15 10:21:46 UARS : UARS-1 : PEM : EDEP : OAHE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:00:50 1992-10-15 10:03:45 UARS : UARS-1 : PEM : EDEP : OAHE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:00:50 1992-10-15 10:03:45 UARS : UARS-1 : PEM : EDEP : OAHP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:00:50 1992-10-15 10:03:45 UARS : UARS-1 : PEM : EDEP : OAHP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:00:50 1992-10-15 10:03:45 UARS : UARS-1 : PEM : EDEP : OAJE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJE Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAJP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Local Solar Time is stored in hours Solar Zenith Angle is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:03 1992-10-15 10:22:19 UARS : UARS-1 : PEM : EDEP : OAME Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:47 1992-10-15 10:45:59 UARS : UARS-1 : PEM : EDEP : OAME Field Trace Elec Position is the geographic location of the field line foot at 100 km. Only electron data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:47 1992-10-15 10:45:59 UARS : UARS-1 : PEM : EDEP : OAMP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:47 1992-10-15 10:21:57 UARS : UARS-1 : PEM : EDEP : OAMP Field Trace Prot Position is the geographic location of the field line foot at 100 km. Only ion data positions included. Field Traced Latitude is stored in degrees Field Traced Longitude is stored in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 60 1992-04-09 12:27:47 1992-10-15 10:21:57 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 0/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 1/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 2/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 3/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 4/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 5/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 6/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 7/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 8/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 9/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 10/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 11/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 12/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 13/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 14/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENBA MEPS/Sensor 15/Bias Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA ZRPU/HEPS1/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA ZRPU/HEPS2/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA ZRPU/LV/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA ZRPU/HVU1/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA ZRPU/HVU2/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA NRPU/HEPS3/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA NRPU/LV/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA NRPU/HVU3/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA PCU/Primary/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA PCU/Redundant/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA PCU/ZEPS/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIA PCU/NEPS/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVU1/30 Volt/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVU2/30 Volt/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVU3/30 Volt/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVPS1/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVPS2/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB HVPS3/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB PPS1/Peak/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB PPS2/Peak/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB PPS3/Peak/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB VME/+19 V/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENIB VME/-19 V/Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS1/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS1/-High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS2/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS2/-High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS3/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS3/-High Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS1/Sweep Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS2/Sweep Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENPA PPS3/Sweep Current Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 32 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA VME Calibration Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZIE1/Command Interval No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZIE2/Command Interval No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NIE/Command Interval No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU1/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU2/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU3/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS1/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS2/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS3/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NEPS/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZEPS/Shutdown Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NEPS/Shutdown Disable Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZEPS/Shutdown Disable Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NRPU/Shutdown Disable Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZRPU/Shutdown Disable Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS1/Output Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS2/Output Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS3/Output Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS1 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS2 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS3 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS4 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS5 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS6 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS7 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA MEPS8 Grid Bias Level Flag No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS1/High Voltage Scale No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS2/High Voltage Scale No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS3/High Voltage Scale No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA CEP/ZIE1/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZIE1/CEP/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA CEP/ZIE2/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZIE2/CEP/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA CEP/NIE/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NIE/CEP/Communications Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NEPS/Shutdown Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZEPS/Shutdown Threshold No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA YAW Manuever No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA CEP/Sync Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA CEP/Frame Sync Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA Hemisphere Of Data No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA Velocity Vector Direction No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU1/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU2/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVU3/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS1/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS2/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HEPS3/Power Satus No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA ZEPS/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA NEPS/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS1/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS2/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA PPS3/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS1/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS3/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENSA HVPS2/Power Status No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 UARS PEM MEPS Low-Voltage Cutoff and Power Settings 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA ZIE1/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA ZIE2/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA NIE/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA PPS1/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA PPS2/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA PPS3/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA HVPS1/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA HVPS2/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA HVPS3/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA NRPU/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA ZRPU/Temperature Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA ZEPS/Temperature Monitor/1 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA ZEPS/Temperature Monitor/2 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA NEPS/Temperature Monitor/1 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA NEPS/Temperature Monitor/2 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENTA VMS/Temperature Monitor/2 No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE1/+5V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE1/+15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE1/-15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE1/Pulse Amp/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE2/+5V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE2/+15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE2/-15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA ZIE2/Pulse Amp/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA NIE/+5V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA NIE/+15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA NIE/-15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA NIE/Pulse Amp/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVU1/+30V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVU2/+30V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVU3/+30V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVPS1/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVPS1/-High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVPS2/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVPS2/-High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA HVPS3/+High/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA CEP/+5V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA CEP/+15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA CEP/-15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVA VME/+15V/Voltage Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB ZIE1/0 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB ZIE1/+5 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB ZIE2/0 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB ZIE2/+5 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB NIE/0 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB NIE/+5 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB CEP/0 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : ENG : ENVB CEP/+5 Volt/Calibration Monitor No description / comments information! Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 1 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1 EP0/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1 EP1/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP2/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP3/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP4/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP5/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP6/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP7/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EP8/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP0/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP1/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP2/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP3/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP4/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP5/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP6/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP7/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EP8/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: EP0/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: EP2/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS4: EP4/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: EP6/Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Cmd/Buf/Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Cmd/Buf/Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Cmd/Buf/Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Bad Ram Load This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Bad Ram Load This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Bad Ram Load This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Bias/Adj/Fail This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Bias/Adj/Fail This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Bias/Adj/Fail This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Bias Arm W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Bias Arm W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Bias Arm W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Bias Off Aftr Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Bias Off Aftr Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Bias Off Aftr Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Invld Bias Arm Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Invld Bias Arm Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Invld Bias Arm Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Invld Bias On Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Invld Bias On Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Invld Bias On Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Invld Mode Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Invld Mode Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Invld Mode Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Mode Cmd W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Mode Cmd W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Mode Cmd W/O Arm This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Unknown Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Unknown Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Unknown Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: New SMAF Bfor Loop This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: New SMAF Bfor Loop This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: New SMAF Bfor Loop This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: New PHA Bfor Accum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: New PHA Bfor Accum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: New PHA Bfor Accum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Bad Chksum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Bad Chksum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Bad Chksum This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: RAM Load Buf Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: RAM Load Buf Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: RAM Load Buf Ovfl This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Addrs-Low Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Addrs-Low Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Addrs-Low Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Addrs-Hi Cmd Seq This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Addrs-Hi Cmd Seq This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Addrs-Hi Cmd Seq This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: RAM Load Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: RAM Load Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: RAM Load Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: EOT Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: EOT Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: EOT Cmd Err This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS1: Unknown RAM Load Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS2: Unknown RAM Load Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDA HEPS3: Unknown RAM Load Cmd This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Level Cntrl/Bias A This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Level Cntrl/Bias A This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Level Cntrl/Bias A This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Bias A Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Bias A Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Bias A Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Level Cntrl/Bias B This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Level Cntrl/Bias B This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Level Cntrl/Bias B This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Bias B Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Bias B Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Bias B Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Level Cntrl/Bias C This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Level Cntrl/Bias C This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Level Cntrl/Bias C This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Bias C Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Bias C Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Bias C Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Level Cntrl/Bias D This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Level Cntrl/Bias D This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Level Cntrl/Bias D This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Bias D Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Bias D Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Bias D Inhibit This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Cal Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Cal Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Cal Enable This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Cal Pulser This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Cal Pulser This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Cal Pulser This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Cal Running/Pending This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Cal Running/Pending This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Cal Running/Pending This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: CPU Mode This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: CPU Mode This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: CPU Mode This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS1: Bias Flag This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS2: Bias Flag This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPDB HEPS3: Bias Flag This virtual contains many of the descrete (single bit) status flags which are associated with the HEPS instrument The sensor, Microcomputer Mode Flags, is an 8 bit word. By translating its value 0x55 to 0x09 we have made it into a 4 bit word. The translation is done prior to writing the data record The following is a list of tables which are in this vidf TABLE 0: Ascii table containing descriptions of the sensor states Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS1: Cmd Cntr This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS2: Cmd Cntr This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS3: Cmd Cntr This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS1: CPU Warm Start Cnt This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS2: CPU Warm Start Cnt This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHA HEPS3: CPU Warm Start Cnt This virtual contains the HEPS relevant counters. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Addr (LSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Addr (MSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte1 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte2 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte3 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte4 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte5 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte6 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte7 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte8 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte9 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS1: Mem Byte10 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Addr (LSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Addr (MSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte1 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte2 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte3 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte4 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte5 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte6 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte7 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte8 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte9 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS2: Mem Byte10 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Addr (LSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Addr (MSB) This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte1 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte2 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte3 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte4 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte5 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte6 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHB HEPS3: Mem Byte7 This virtual contains the HEPS memory dump data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/DP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/EP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1 Anti-coin The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T1/EOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/DP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/EP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2 Anti-coin The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS1: T2/EOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/DP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/EP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1 Anti-coin The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T1/EOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/DP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/EP Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2 Anti-coin The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHC HEPS2: T2/EOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T1/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T1/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T1/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T1/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T2/DE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T2/EE Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T2/EPrime Singles The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHD HEPS3: T2/DOV1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 cnts/accum Sweep 0 150 cnts/sec Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 8 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: Main PS/I The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: Main PS/I The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: Main PS/I The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: +9V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: +9V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: +9V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: -5V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: -5V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: -5V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: +5V Analog Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: +5V Analog Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: +5V Analog Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: +5V Digital Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: +5V Digital Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: +5V Digital Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: +5V Ref Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: +5V Ref Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: +5V Ref Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: +26V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: +26V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: +26V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: LEP Low V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: LEP Low V Mon. The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: D Bias Mon1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: D Bias Mon1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: D Bias Mon2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: D Bias Mon2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: E Bias Mon1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: E Bias Mon1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: E Bias Mon1 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: E Bias Mon2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: E Bias Mon2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: E Bias Mon2 The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: Head2 Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: Head2 Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: Head2 Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: LEP Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: LEP Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: Head1 Bsplt Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: Top Plt BIPS Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: Top Plt BIPS Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: Top Plt BIPS Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: Bot LV Mod Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: Bot LV Mod Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS3: Bot LV Mod Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS1: MthrBrd Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHE HEPS2: MthrBrd Temp The following is a list of tables which are in this vidf TABLE 0: telemetry decom table to volts, milliamps, or degrees centigrade depending on whether the sensor contains voltage, current, or tempeature data The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sweep 0 0 (volts, milliamps, degC) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 16 1991-09-15 01:57:24 2005-08-23 12:33:52 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP0 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP1 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP2 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP3 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP4 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP5 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP6 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP7 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP8 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP0 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP1 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP2 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP3 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP4 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP5 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP6 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP7 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP8 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP0 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP2 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP4 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP6 Pileup Reg This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP0 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP1 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP2 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP3 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP4 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP5 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP6 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP7 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP8 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP0 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP1 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP2 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP3 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP4 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP5 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP6 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP7 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP8 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP0 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP2 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP4 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP6 Low Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP0 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP1 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP2 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP3 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP4 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP5 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP6 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP7 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS1: EP8 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP0 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP1 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP2 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP3 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP4 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP5 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP6 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP7 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS2: EP8 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP0 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP2 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP4 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPHF HEPS3: EP6 Hi Thresh This virtual contains the HEPS threshold and pulse pileup data. There are no tables associated with this virtual Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 david@dews1.space.swri.edu 4 1991-09-15 01:56:59 2005-08-23 12:33:27 UARS : UARS-1 : PEM : HEPS : HPSA HEPS1/e-: T1/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS1/e-: T1/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS1/e-: T2/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS1/e-: T2/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS2/e-: T1/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS2/e-: T1/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS2/e-: T2/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSA HEPS2/e-: T2/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temprature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: background spectra (cnts/sec) TABLE 20: Poisson error in the background spectra TABLE 21: threshold count TABLE 22: False Proton Count Rate (cnts/sec) The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (sec) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 8,9 0,1 total-Tel. cnts/accum Sweep 17,18 0.1 total-Sen. cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19 0 Background (cnts/sec) Sweep 20 0 Bkgnd Err. (cnts/sec) Sweep 22 0 false Prot (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 1,3,4 Sweep 0,3,22 0,154,2 P cnts/sec Sweep 0,3,19 0,154,2 B cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22 1,3,4,2 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19 1,3,4,2 Sweep 0,3,22,19 0,154,2,2 K cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19 1,3,4,2,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 1,3,4,4,3,4 Sweep 0,3,22,4,1,2 0,154,2,4,3,4 P cnts/(cm**2-str-s) Sweep 0,3,19,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2 3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K cnts/(cm**2-str-s) 1,2 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 1,3,4,4,4 Sweep 0,3,22,4,2 0,154,2,4,4 P cnts/(cm**2-str-s-eV) Sweep 0,3,19,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 2 4 Sweep 8,9,10,11,12, 0,1,153,61,3, J cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 2 4 Sweep 0,3,22,19,4,2 0,154,2,2,4,4 K cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, F cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,2 2,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4, 1,3,4,4, 2,5 4,3 Sweep 0,3,22,4,2,5 0,154,2,4,4,3 P ergs/(cm**2-str-s-eV) Sweep 0,3,19,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, I ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 4,2,5 4,4,3 Sweep 8,9,10,11,12, 0,1,153,61,3, J ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19, 1,3,4,2, 4,2,5 4,4,3 Sweep 0,3,22,19,4, 0,154,2,2,4,4 K ergs/(cm**2-str-s-eV) 2,5 3 Sweep 8,9,10,11,12, 0,1,153,61,3, F ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,19, 1,3,4,2,2, 4,2,5 4,4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 8,9,10,11,12, 0,1,153,61,3, L sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 1,3,4,4,3, 2,7,6 4,3,4 Sweep 0,3,22,4,1,2, 0,154,2,4,3,4, P sec**3/km**6 7,6 3,4 Sweep 0,3,19,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, I sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, J sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,19,4, 1,3,4,2,4, 1,2,7,6 3,4,3,4 Sweep 0,3,22,19,4, 0,154,2,2,4 K sec**3/km**6 1,2,7,6 3,4,3,4 Sweep 8,9,10,11,12, 0,1,153,61,3, F sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,22, 1,3,4,2, 19,4,1,2,7,6 2,4,3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time P means that operations occur on the data corrected for false Protons B means that operations occur on the data corrected for Background I means that operations occur on the data corrected for live time and false protons J means that operations occur on the data corrected for live time and background K means that operations occur on the data corrected for false protons and background F means that operations occur on the Fully corrected data Quality fields are bit oriented and their valies combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Spectra 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info Definitions for cal set 9, False Proton Fit Type, are as follows: 0 = not enough data points to do a fit 1 = unrecoverable error during fitting 2 = force fit to a power law 3 = force fit to an exponential 4 = selected power law fit 5 = selected exponential fit The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Zenith Electron Data 16 1991-09-15 01:57:11 2005-08-23 01:22:37 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS1/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2: LEP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T1/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/DP This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP1 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSB HEPS2/p+: T2/EP2 This VIDF has the 28 March 1994 revised center energies, channel widths and efficiencies The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: threshold count level TABLE 9: negative of energy processor repolling time (sec) TABLE 10: constant value (1) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time polynomial scale TABLE 15: telescope live time polynomial offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: background spectra (cnts/sec) TABLE 18: Poisson error in the background spectra (cnts/sec) TABLE 19: telescope total count LSB multiplier TABLE 20: telescope total count MSB multiplier TABLE 21: sensor total count LSB multiplier TABLE 22: sensor total count MSB multiplier The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 19,20,9,10, 0,1,152,21, LEP live time (s) 9,19, 134,1000, 20,-1 1001,2003 Sweep 19,20,9,11,12, 0,1,153,61,3, Tel. live time (s) 13,9,19, 21,134,1000, 20,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 19,20 0,1 R total-Tel. cnts/accum Sweep 21,22 0,1 R total-Sen. cnts/accum Sweep 17 0 Background (cnts/sec) Sweep 18 0 Bkgnd Err. (cnts/sec) Sweep 0,3 0,154 R cnts/sec Sweep 0,3,17 0,154,2 B cnts/sec Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/sec 9,19, 134,1000, 20,-1,0,3 1001,2133,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/sec 13,9,19 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/sec 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17 4,2 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/sec 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17 131,3,4,2 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 0,3,17,4,1,2 0,154,2,4,3,4 B cnts/(cm**2-str-s) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2 4,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2 4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2 4,1,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17, 131,3,4,1, 4,1,2 4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 0,3,17,4,2 0,154,2,4,4 B cnts/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2 4,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 19,20,9,10, 0,1,153,21, F LEP cnts/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2 4,1,4,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel cnts/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2 4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 0,3,17,4,2,5 0,154,2,4,4,3 B ergs/(cm**2-str-s-eV) Sweep 19,20,9,10, 0,1,153,21, L LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,2,5 4,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,2, 131,3,4,4,4, 5 3 Sweep 19,20,9,10, 0,1,153,21, F LEP ergs/(cm**2-str-s-eV) 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,2,5 4,2,4,4,3 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel ergs/(cm**2-str-s-eV) 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 2,5 4,3 Sweep 0,3,4,1,2,7,6 0,154,4,3,4,3,4 R sec**3/km**6 Sweep 0,3,17,4,1,2, 0,154,2,4,3,4, B sec**3/km**6 7,6 3,4 Sweep 19,20,9,10, 0,1,153,21, L LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,4,1,2,7,6 4,4,3,4,3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,6 4,3,4 Sweep 19,20,9,10, 0,1,153,21, F LEP sec**3/km**6 9,19, 134,1000, 20,-1,0, 1001,2133,3, 3,17,4,1,2, 4,2,4,3,4, 7,6 3,4 Sweep 19,20,9,11,12, 0,1,153,61,3, F Tel sec**3/km**6 13,9,19, 21,134,1000, 20,-1,14, 1001,2003,3, 15,0,3,17,4, 131,3,4,2,4, 1,2,7,6 3,4,3,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time B means that operations occur on the data corrected for Background F means that operations occur on the Fully corrected data Quality fielsd are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No fill data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 45 keV Zenith Proton Data 4 1991-09-15 01:56:59 2005-08-23 01:22:24 UARS : UARS-1 : PEM : HEPS : HPSC HEPS3/e-: T1/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time scale (sec) TABLE 15: telescope live time offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: threshold sensor level The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (s) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 8,9 0,1 R total-Tel. cnts/accum Sweep 17,18 0,1 R total-Sen. cnts/accum Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 131,3,4,4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2,5 131,3,4,4,4,3 Sweep 0,3,4,1,2,7, 0,154,4,3,4,3, R sec**3/km**6 5,5 4,4 Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,5,5 4,3,4,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time Quality fields are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. As of 8-4-94, LPARL has not defined background, false proton, or count rate limitations on the DE sensor. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Nadar Electron Data 4 1991-09-15 01:56:59 2001-05-17 05:50:12 UARS : UARS-1 : PEM : HEPS : HPSC HEPS3/e-: T1/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time scale (sec) TABLE 15: telescope live time offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: threshold sensor level The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (s) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 8,9 0,1 R total-Tel. cnts/accum Sweep 17,18 0,1 R total-Sen. cnts/accum Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 131,3,4,4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2,5 131,3,4,4,4,3 Sweep 0,3,4,1,2,7, 0,154,4,3,4,3, R sec**3/km**6 5,5 4,4 Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,5,5 4,3,4,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time Quality fields are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. As of 8-4-94, LPARL has not defined background, false proton, or count rate limitations on the DE sensor. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Nadar Electron Data 4 1991-09-15 01:56:59 2001-05-17 05:50:12 UARS : UARS-1 : PEM : HEPS : HPSC HEPS3/e-: T2/DE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time scale (sec) TABLE 15: telescope live time offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: threshold sensor level The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (s) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 8,9 0,1 R total-Tel. cnts/accum Sweep 17,18 0,1 R total-Sen. cnts/accum Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 131,3,4,4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2,5 131,3,4,4,4,3 Sweep 0,3,4,1,2,7, 0,154,4,3,4,3, R sec**3/km**6 5,5 4,4 Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,5,5 4,3,4,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time Quality fields are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. As of 8-4-94, LPARL has not defined background, false proton, or count rate limitations on the DE sensor. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Nadar Electron Data 4 1991-09-15 01:56:59 2001-05-17 05:50:12 UARS : UARS-1 : PEM : HEPS : HPSC HEPS3/e-: T2/EE The following is a list of tables which are in this vidf TABLE 0: telemetry decom table TABLE 1: center energies (eV) TABLE 2: energy channel widths (eV) TABLE 3: detector efficiencies TABLE 4: geometry factors (cm**2-str) TABLE 5: center energies (ergs) TABLE 6: q*(center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: telescope total count LSB multiplier TABLE 9: telescope total count MSB multiplier TABLE 10: negative of energy processor repolling time (sec) TABLE 11: maximum energy processor fill TABLE 12: energy processor fulness adjustment TABLE 13: energy processor difference term TABLE 14: telescope live time scale (sec) TABLE 15: telescope live time offset (sec) TABLE 16: temperature decompression polynomial (deg C) TABLE 17: sensor total count LSB multiplier TABLE 18: sensor total count MSB multiplier TABLE 19: threshold sensor level The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 1 0 eV (center) Scan 2 0 eV (widths) Sweep 8,9,10,11,12, 0,1,153,61,3, Tel. live time (s) 13,10,8, 21,134,1000, 9,-1,14,15 1001,2003,3,1 Sweep 16 0 Temperature (deg C) Sweep 0 0 R cnts/accum Sweep 0,3 0,4 R cnts/accum (eff. cor) Sweep 8,9 0,1 R total-Tel. cnts/accum Sweep 17,18 0,1 R total-Sen. cnts/accum Sweep 0,3 0,154 R cnts/sec Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/sec 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3 131,3,4 Sweep 0,3,4,1,2 0,154,4,3,4 R cnts/(cm**2-str-s) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1,2 131,3,4,4,3,4 Sweep 0,3,4,2 0,154,4,4 R cnts/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel cnts/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2 131,3,4,4,4 Sweep 0,3,4,2,5 0,154,4,4,3 R ergs/(cm**2-str-s-eV) Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel ergs/(cm**2-str-s-eV) 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,2,5 131,3,4,4,4,3 Sweep 0,3,4,1,2,7, 0,154,4,3,4,3, R sec**3/km**6 5,5 4,4 Sweep 8,9,10,11,12, 0,1,153,61,3, L Tel sec**3/km**6 13,10,8, 21,134,1000, 9,-1,14, 1001,2003,3, 15,0,3,4,1, 131,3,4,4,3, 2,7,5,5 4,3,4,4 R means that operations occur on the uncorrected Raw data L means that operations occur on the data corrected for Live time Quality fields are bit oriented and their values combine. Bit assignments are as follows (of course, a zero means good quality - No Fill Data): Bit Dec Quality Flag Meaning 0 1 Fill Data With Energy Sweep 1 2 Possible Fill Data With Energy Sweep 2 4 Fill And Possible Fill Data With Energy Sweep 3 8 Solar Contaminated Sensor 4 16 Exceeded Total Count for Telescope 5 32 Exceeded Total Count for Sensor 6 64 Unknown State - Not Enough Info The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. As of 8-4-94, LPARL has not defined background, false proton, or count rate limitations on the DE sensor. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM HEPS greater than 30 keV Nadar Electron Data 4 1991-09-15 01:56:59 2001-05-17 05:50:12 UARS : UARS-1 : PEM : MEPS : MPSA ISensor 3: 6.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith (6.3 & 66.3 deg) Proton Data 32 1991-09-15 01:57:16 2005-08-23 12:34:49 UARS : UARS-1 : PEM : MEPS : MPSA ISensor 9: 66.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith (6.3 & 66.3 deg) Proton Data 32 1991-09-15 01:57:16 2005-08-23 12:34:49 UARS : UARS-1 : PEM : MEPS : MPSB ESensor 0: -23.7 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. CONST 4: Thees are the FWHM in the azimuth direction of the sensor's aperature CONST 5: Thees are the initial elevation angle of the sensor's aperature in spacecraft coordinates. CONST 6: Thees are the final elevation angle of the sensor's aperature in spacecraft coordinates. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith Electron Data 32 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSB ESensor 2: 6.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. CONST 4: Thees are the FWHM in the azimuth direction of the sensor's aperature CONST 5: Thees are the initial elevation angle of the sensor's aperature in spacecraft coordinates. CONST 6: Thees are the final elevation angle of the sensor's aperature in spacecraft coordinates. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith Electron Data 32 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSB ESensor 4: 21.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. CONST 4: Thees are the FWHM in the azimuth direction of the sensor's aperature CONST 5: Thees are the initial elevation angle of the sensor's aperature in spacecraft coordinates. CONST 6: Thees are the final elevation angle of the sensor's aperature in spacecraft coordinates. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith Electron Data 32 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSB ESensor 6: 36.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. CONST 4: Thees are the FWHM in the azimuth direction of the sensor's aperature CONST 5: Thees are the initial elevation angle of the sensor's aperature in spacecraft coordinates. CONST 6: Thees are the final elevation angle of the sensor's aperature in spacecraft coordinates. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith Electron Data 32 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSB ESensor 8: 66.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 3: Thees are the azimuth angle of the sensor's aperature in spacecraft coordinates. CONST 4: Thees are the FWHM in the azimuth direction of the sensor's aperature CONST 5: Thees are the initial elevation angle of the sensor's aperature in spacecraft coordinates. CONST 6: Thees are the final elevation angle of the sensor's aperature in spacecraft coordinates. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith Electron Data 32 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSC ESensor 10: 126.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Nadar Electron Data 48 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSC ESensor 12: 156.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Nadar Electron Data 48 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSC ESensor 14: -158.7 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Nadar Electron Data 48 1991-09-15 01:57:16 2005-08-23 01:21:36 UARS : UARS-1 : PEM : MEPS : MPSD ISensor 5: 21.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith (21.3 deg) Proton Data 32 1991-09-15 01:57:16 2005-08-23 12:34:49 UARS : UARS-1 : PEM : MEPS : MPSE ISensor 1: -23.7 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith (-23.7 & 36.3 deg) Proton Data 32 1991-09-15 01:57:16 2005-08-23 12:34:49 UARS : UARS-1 : PEM : MEPS : MPSE ISensor 7: 36.3 deg The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: telemetry decom table TABLE 2: detector efficiencies TABLE 3: geometry factors (cm**2-str) TABLE 4: dE/E TABLE 5: center energies (ergs) TABLE 6: (center energies)**2 (ergs**2) TABLE 7: constant needed in going to dist. fn TABLE 8: Threshold cound level TABLE 9: Dark count level TABLE 10: Amplifier Dead Time Factor TABLE 11: ascii descriptions of status states The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cnts/accum Sweep 1,2 0,4 cnts/accum (eff. cor) Sweep 1,2 0,154 cnts/sec Sweep 1,2,3,4 0,154,4,4 cnts/(cm**2-str-s) Sweep 1,2,3,4,0 0,154,4,4,4 cnts/(cm**2-str-s-eV) Sweep 1,2,3,4,0,5 0,154,4,4,4,3 ergs/(cm**2-str-s-eV) Sweep 1,2,3,4,7,6 0,154,4,4,3,4 sec**3/km**6 The following is a list of constant values which are in this vidf CONST 0: These are the X components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 1: These are the Y components of each sensor's aperature expressed relative to the PEM magnetometer. CONST 2: These are the Z components of each sensor's aperature expressed relative to the PEM magnetometer. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78284 david@dews1.space.swri.edu UARS PEM HEPS less than 30 keV Zenith (-23.7 & 36.3 deg) Proton Data 32 1991-09-15 01:57:16 2005-08-23 12:34:49 UARS : UARS-1 : PEM : VMAG : VMMA PEM/Bx This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA PEM/By This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA PEM/Bz This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/A/Bx This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/A/By This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/A/Bz This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/B/Bx This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/B/By This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA SAT/B/Bz This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/A/Ix This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/A/Iy This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/A/Iz This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/B/Ix This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/B/Iy This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMA Tor/B/Iz This virtual contains both the science and aspect magnetometer data. Also included are the torquer bar currents The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which converts sensor 0-8 data to gauss and sensor 9-14 to milliamps TABLE 1: Polynomial coefficients which converts sensor 0-8 data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensors (0-9) 0 0 gauss Sensors (0-9) 1 0 nanotesla Sensors (10-15) 0 0 milliamps Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's DC Magnetic Field 32 1991-09-15 01:57:16 2005-08-23 03:05:21 UARS : UARS-1 : PEM : VMAG : VMMB AC/Bx This virtual contains both the science magnetometer AC data The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which convert the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 1 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's AC Magnetic Field 16 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : VMAG : VMMB AC/By This virtual contains both the science magnetometer AC data The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which convert the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 1 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's AC Magnetic Field 16 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : PEM : VMAG : VMMB AC/Bz This virtual contains both the science magnetometer AC data The following is a list of tables which are in this vidf TABLE 0: Polynomial coefficients which convert the sensor data to nanotesla The following are units which can be derived from the tables. The format is to give the tables applied followed by the operations and unit definition DATA TYPE TABLES OPERS UNIT Sensor 1 0 nanotesla Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-510 david@dews1.space.swri.edu UARS PEM VMAG Measurement of the Earth's AC Magnetic Field 16 1991-09-15 01:57:16 2005-08-23 12:33:44 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/Solar/Dist Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/H-I/121.56/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/H-I/121.56/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/O-I/130.217/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/O-I/130.217/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/C-IV/154.818/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/C-IV/154.818/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/C-I/156.134/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/C-I/156.134/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/C-I/165.627/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/C-I/165.627/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/Mg-II/Core-Wing Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/Mg-II/Core-Wing Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/Ca-II/Core-Wing Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP Std Dev/SOLSTICE/Uncor/Ca-II/Core-Wing Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/Carrington/Longitude Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAP SOLSTICE/Uncor/Carrington/Latitude Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAS SOLSTICE/Uncorrected Solar Spec The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3AS : SOAS SOLSTICE/Std Dev Uncor Solar Spec The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-06 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/Mean Solar Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/H-I/121.56/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/H-I/121.56/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/O-I/130.217/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/O-I/130.217/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/C-IV/154.818/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/C-IV/154.818/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/C-I/156.134/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/C-I/156.134/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/C-I/165.627/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/C-I/165.627/Int Em Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/Mg-II Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/Mg-II Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/Ca-II Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP Std Dev/SOLSTICE/Ca-II Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/Carrington Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBP SOLSTICE/Carrington Data paramaters have a variety of units. They are stored in different units in the data file. SOLSTICE distances are stored in AU. Line Intensity values are integrated quantities and are in units of Watts-nm/m**3. With some math, they can be converted to the Integrated Photon Flux. Core-to-Wing Ratios are unitless quantities. Carrington position has units of degrees. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Parameter Data 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBS SOLSTICE/Solar Spectrum The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Spectrum (approximately 115 nm to 425 nm) 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SOLSTICE : LEVEL_3BS : SOBS SOLSTICE/Std Dev Solar Spectrum The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SOLSTICE Solar Spectrum (approximately 115 nm to 425 nm) 1 1991-10-03 12:00:00 1999-12-31 12:00:00 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AABP AA Bus Engineering Current This file contains the power monitors of the Auxiliary Solar Array Bus. Table 0 are the polynomial coefficients to convert the raw telemetry into engineering units. Sensor 0 is the auxiliary array current in amps and Sensor 1 is the auxiliary array potential in volts. Type Tables Opers Units Sweep 0 0 Current (Amp) Sweep 0 0 Potential (Volts) All data are scalar. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Power Monitors 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AABP AA Bus Voltage This file contains the power monitors of the Auxiliary Solar Array Bus. Table 0 are the polynomial coefficients to convert the raw telemetry into engineering units. Sensor 0 is the auxiliary array current in amps and Sensor 1 is the auxiliary array potential in volts. Type Tables Opers Units Sweep 0 0 Current (Amp) Sweep 0 0 Potential (Volts) All data are scalar. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Power Monitors 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 1 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 2 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 3 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 4 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 5 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 6 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 7 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 8 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 9 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 10 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 11 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : AASS AAS Shunt 13 Auxiliary Solar Array Switch Shunts indicate the amount of voltage being supplied to the UARS batteries. Table 0 is an ASCII look-up table to supply whether the shunt it on )meaning that this portion of the Auxiliary Solar Array is shorted) or off (meaning that the shunt is open and the battery is receiving power). Table 0 contains an ASCII table of status text. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Auxiliary Solar Array Switch Shunts 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : MABP SA Bus Current CS-1 This file contains the power monitors for the Main Solar Array Bus which supplies the science instruments. Table 0 are the polynomial coefficients to convert the raw telemetry into engineering units. Sensors 0 and 1 are the main solar bus current monitors expressed in amps. Sensor 2 is the main array bus potential in volts. Type Tables Opers Units Sweep 0 0 Current (Amp) Sweep 0 0 Potential (Volts) All data are scalar. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Main Solar Array Power Monitors 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : MABP SA Bus Current CS-2 This file contains the power monitors for the Main Solar Array Bus which supplies the science instruments. Table 0 are the polynomial coefficients to convert the raw telemetry into engineering units. Sensors 0 and 1 are the main solar bus current monitors expressed in amps. Sensor 2 is the main array bus potential in volts. Type Tables Opers Units Sweep 0 0 Current (Amp) Sweep 0 0 Potential (Volts) All data are scalar. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Main Solar Array Power Monitors 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SPACECRAFT : SOLAR_ARRAY : MABP SA Bus Voltage This file contains the power monitors for the Main Solar Array Bus which supplies the science instruments. Table 0 are the polynomial coefficients to convert the raw telemetry into engineering units. Sensors 0 and 1 are the main solar bus current monitors expressed in amps. Sensor 2 is the main array bus potential in volts. Type Tables Opers Units Sweep 0 0 Current (Amp) Sweep 0 0 Potential (Volts) All data are scalar. Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS Main Solar Array Power Monitors 8 1991-09-15 12:53:01 2005-12-14 12:07:57 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/Solar/Dist Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/H-I/121.564/Inten Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/O-I/130.42/Inten Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/C-II/133.505/Inten Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/C-IV/154.819/Inten Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/Al/Edge Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/Mg-II/Absorp Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAP SUSIM/Uncor/Ca-II/Absorp Ratio Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAS SUSIM/Uncorrected Solar Spectrum The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3AS : SUAS SUSIM/Std Dev Uncor Solar Spec The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 1 1991-11-09 12:00:00 1993-11-13 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/Mean Solar Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/H-I/121.564 Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/O-I/130.42 Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/C-II/133.505 Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/C-IV/154.819 Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/Aluminum Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/Mg-II Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/Ca-II Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBP SUSIM/GSFC Collection Data paramaters have a variety of units. They are stored in different units in the data file. SUSIM distances are stored in km. Line Intensity values are integrated quantities and are in units of milliWatts/m**2. With some math, they can be converted to the Integrated Photon Flux. Edge Ration and Absorption Ration are unitless quantities. Line Intensities are converted to the Integrated Photon Flux with the following tables: Table 00: Conversion between m**2 and cm**2 Table 01: Conversion between Joule and erg Table 02: Conversion between Line Intensity and Photon Flux TYPE TABLES OPERS UNITS Scan 2 3 Integrated Photon Flux (photons/(cm**2-sec)) stored in km. Line Intensity values are integrated Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Parameter Data 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBS SUSIM/Solar Spectrum The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Spectrum (approximately 115 nm to 425 nm) 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : SUSIM : LEVEL_3BS : SUBS SUSIM/Std Dev Solar Spectrum The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to nanometers). Data is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). These units are Irradiance, or Flux/wavelength. Table 00: Wavelength Lookup Table (nm) Table 01: Conversion from nanometers to Angstroms Table 02: Conversion from nanometers to centimeters Table 03: Conversion from nanometers to meters Table 04: Conversion from meters**3 to centimeters**3 Table 05: Conversion from energy in Joule to energy in erg Table 06: Conversion from wavelength in meters to frequency in Hertz Table 07: Conversion from frequency in Hertz to energy in Joule Table 08: Conversion from energy in erg to energy in keV Table 09: Conversion from energy in keV to energy in eV Table 10: Photon conversion factor Storage: Scan references UARS wavelength bin number Sweep is stored in Watts/(m**2-m) or Joule/(sec-m**2-m). TYPE TABLES OPERS UNITS Sweep 0 0 Wavelength (nm) Sweep 0,1 0,3 Wavelength (Angstrom) Sweep 0,2 0,3 Wavelength (cm) Sweep 0,3 0,3 Wavelength (m) Sweep 0,3,6 0,3,134 Frequency (Hz) Sweep 0,3,6,7 0,3,134,3 Energy (Joule) Sweep 0,3,6,7,5 0,3,134,3,3 Energy (erg) Sweep 0,3,6,7,5,8 0,3,134,3,3,4 Energy (keV) Sweep 0,3,6,7,5,8,9 0,3,134,3,3,4,3 Energy (eV) Scan 4 3 Irradiance (J/(sec-cm**2-cm)) or Irradiance (Watt/cm**2-cm) Scan 5 3 Irradiance (erg/(sec-m**2-m)) Scan 4,5 3,3 Irradiance (erg/(sec-cm**2-cm)) Scan 10,0 3,3 Photon Irradiance (photons/(sec-cm**2-nm)) Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS SUSIM Solar Spectrum (approximately 115 nm to 425 nm) 1 1991-10-12 12:00:00 2005-08-01 12:00:00 UARS : UARS-1 : WINDII : LEVEL_3AT : LWMA Latitude/WINDII/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Meridional Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWMA Longitude/WINDII/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Meridional Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWMA LST/WINDII/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Meridional Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWMA SZA/WINDII/MA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Meridional Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWZA Latitude/WINDII/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Zonal Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWZA Longitude/WINDII/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Zonal Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWZA LST/WINDII/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Zonal Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : LWZA SZA/WINDII/ZA Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for Zonal Winds 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : OAWT Latitude/WINDII/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : OAWT Longitude/WINDII/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : OAWT LST/WINDII/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : OAWT SZA/WINDII/TMP Position is the geographic location of the foot of the limb viewing point. Limb View Latitude is in degrees Limb View Longitude is in degrees Local Solar Time is in hours Solar Zenith Angle is in degrees Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Earth Pointing Position for the Atmospheric Temperature 60 1991-11-06 01:26:42 1993-11-13 11:06:37 UARS : UARS-1 : WINDII : LEVEL_3AT : WIMA WINDII/Meridional/Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Meridional Winds 1 1991-11-06 01:26:10 1993-11-13 11:06:04 UARS : UARS-1 : WINDII : LEVEL_3AT : WIMA Std Dev WINDII Merid Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Meridional Winds 1 1991-11-06 01:26:10 1993-11-13 11:06:04 UARS : UARS-1 : WINDII : LEVEL_3AT : WIZA WINDII/Zonal/Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Zonal Winds 1 1991-11-06 01:26:10 1993-11-13 11:06:04 UARS : UARS-1 : WINDII : LEVEL_3AT : WIZA Std Dev WINDII Zonal Wind The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of meters/second. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from meters to centimeters Table 2: Conversion from meters to killometers Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of m/s DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 cm/s Sweep 2 3 km/s Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Zonal Winds 1 1991-11-06 01:26:10 1993-11-13 11:06:04 UARS : UARS-1 : WINDII : LEVEL_3AT : WTMA WINDII Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Atmospheric Temperature Profile 1 1991-11-06 01:26:10 1993-11-13 11:06:04 UARS : UARS-1 : WINDII : LEVEL_3AT : WTMA Std Dev WINDII Atm Temp The conversion to various units is accomplished by the application of different sets of look up tables. This is described below (note table 0 converts sweep step to km). Data values are stored in units of degrees Kelvin, the absolute temperature. Table 0: UARS Altitudes for the reporting bins Table 1: Conversion from degrees K to degrees C Table 2: Conversion from degrees C to degrees F Table 3: Altitude converted Pressure Levels Table 4: Altitude converted Geopotential Heights Storage: Scan references UARS altitude bin number Sweep is stored in units of degrees K DATA TYPE TABLES OPERS UNIT Scan 0 0 Altitude (km) Scan 3 0 Pressure (mbar) Scan 4 0 Geopotential Altitude (km) Sweep 1 3 degrees C Sweep 1,2 3,0 degrees F Dr. J. David Winningham Southwest Research Institute 6220 Culebra Road San Antonio, Texas 78228-0510 UARS WINDII Atmospheric Temperature Profile 1 1991-11-06 01:26:10 1993-11-13 11:06:04 VIKING : VIKING : OA : ATTITUDE : ATTITUDE RA VIKING:VIKING:OA:ATTITUDE:ATTITUDE This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-22 07:00:00 1986-02-22 07:00:00 VIKING : VIKING : OA : ATTITUDE : ATTITUDE Declination VIKING:VIKING:OA:ATTITUDE:ATTITUDE This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-22 07:00:00 1986-02-22 07:00:00 VIKING : VIKING : OA : ATTITUDE : ATTITUDE Spin period VIKING:VIKING:OA:ATTITUDE:ATTITUDE This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-22 07:00:00 1986-02-22 07:00:00 VIKING : VIKING : OA : ORBIT : ORBIT Altitude VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT CGLat VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT CGLong VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT Latitude VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT Longitude VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT MLT VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT L-shell VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBIT Invariant Latitude VIKING:VIKING:OA:ORBIT:ORBIT This virtual consists of orbital data for the Viking S/C. Olle Norberg Swedish Institute of Space Physics P.O. Box 812 SE-981 28 Kiruna, Sweden Olle.Norberg@irf.se 1 1986-02-23 12:00:00 1986-02-23 12:00:00 VIKING : VIKING : OA : ORBIT : ORBITNR ORBIT VIKING:VIKING:OA:ORBIT:ORBITNR This virtual consists of orbit number data Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 1 1986-02-22 12:00:00 1986-02-22 12:00:00 VIKING : VIKING : V2 : MAG : MAG Bx VIKING:VIKING:V2:V2:MAG This virtual consists of data from the magnetometer 1 mounted on Viking. The x- y-, and z-components of the magnetic field are measured. Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:07:07 1987-05-12 07:48:17 VIKING : VIKING : V2 : MAG : MAG By VIKING:VIKING:V2:V2:MAG This virtual consists of data from the magnetometer 1 mounted on Viking. The x- y-, and z-components of the magnetic field are measured. Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:07:07 1987-05-12 07:48:17 VIKING : VIKING : V2 : MAG : MAG Bz VIKING:VIKING:V2:V2:MAG This virtual consists of data from the magnetometer 1 mounted on Viking. The x- y-, and z-components of the magnetic field are measured. Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:07:07 1987-05-12 07:48:17 VIKING : VIKING : V3 : V3-1 : ESP1 VIKING ESP1 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: (geometric factor = 3,74E6)/energy_level The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-1 : ESP1c VIKING ESP1up, 1keV corrected Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: (geometric factor = 3,74E6)/energy_level The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 4 1986-03-05 01:17:43 1986-11-11 12:40:52 VIKING : VIKING : V3 : V3-1 : ESP1s VIKING ESP1, sun pulse corrected data Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: (geometric factor = 3,74E6)/energy_level The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-08-23 04:12:59 1986-10-21 03:38:14 VIKING : VIKING : V3 : V3-1 : ESP1up VIKING ESP1up Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: (geometric factor = 3,74E6)/energy_level The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 4 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-1 : ESP1ups VIKING ESP1up, sun pulse corrected Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: (geometric factor = 3,74E6)/energy_level The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 4 1986-03-13 07:42:37 1986-11-11 12:40:52 VIKING : VIKING : V3 : V3-1 : ESP2 ESP2 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP2 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:06:29 1987-02-24 11:26:29 VIKING : VIKING : V3 : V3-1 : ESP2_3 ESP2_3 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP2_3 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-1 : ESP3 ESP3 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP3 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:06:25 1987-02-25 03:39:10 VIKING : VIKING : V3 : V3-2 : ESP4 VIKING, ESP4 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP4 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden Email: ingrid&irf.se 16 1986-02-23 12:07:07 1987-05-12 07:48:17 VIKING : VIKING : V3 : V3-2 : ESP5 VIKING, ESP5 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ESP5 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 16 1986-02-23 12:07:07 1987-05-12 07:48:17 VIKING : VIKING : V3 : V3-3 : PISP1 VIKING, PISP1 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the PISP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-02-23 12:06:23 1987-02-25 03:49:21 VIKING : VIKING : V3 : V3-3 : PISP1up VIKING PISP1up Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the PISP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 4 1986-02-23 12:06:23 1987-02-25 03:49:21 VIKING : VIKING : V3 : V3-3 : PISP1ups VIKING PISP1up, sun pulse corrected data Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the PISP1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 4 1986-02-23 12:06:23 1987-02-25 03:49:21 VIKING : VIKING : V3 : V3-3 : PISP2 VIKING PISP2 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the PISP2 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) TABLE 3: band width for center energies The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions. DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-03-05 01:17:43 1987-02-13 01:00:59 VIKING : VIKING : V3 : V3-3 : PISP2s VIKING PISP2, sun pulse corrected data Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the PISP2 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: 1/(cm**2-str-s-eV) TABLE 3: band width for center energies The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions. DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 8 1986-03-05 01:17:43 1987-02-13 01:00:59 VIKING : VIKING : V3 : V3-4 : SECPISP VIKING SEC1 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC2 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC3 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC4 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC5 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC6 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC7 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-4 : SECPISP SEC8 Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the SECPISPdetector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 H+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 2.H+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 He2+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 2.He2+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 He+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 2.He+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 O+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS1 2.O+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 H+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 2.H+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 He2+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 2.He2+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 He+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 2.He+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 O+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03 VIKING : VIKING : V3 : V3-5 : ICS2 2.O+ Note the following: The zero degree position in azimuthal spin is defined as the condition when the normal to the ICS1 detector apertures lie within the plane containing the magnetic field vector. Under this definition the satellite spin rate may show variations which are linked to changes in direction fo the field vector , i.e. the spin rate is determined in a "non-inertial" reference frame. A complete description of the instrument can be found in: The Hot Plasma Spectrometers on Viking by Ingrid Sandahl et al. The following is a list of tables which are in this vidf TABLE 0: center energies (eV) TABLE 1: N = (A + 16) * 2**B - 16, uncompress data values TABLE 2: cts/(cm**2-str-s-eV) The folloing are units which can be derived from the tables The format is to give the tables applied followed by the operations unit definitions DATA TYPE TABLES OPERS UNIT Scan 0 0 eV Sweep 1 0 cts/accum Sweep 1,2 0,3 cts/(cm**2-str-s-eV) Ingrid Sandahl Swedish Institute of Space Physics (IRF) P. O. Box 812 S-98128 Kiruna, Sweden E-mail: Ingrid@irf.se 2 1986-02-23 12:06:25 1987-02-25 03:39:03